jntu aeronautical engineering r05 syllabus book
TRANSCRIPT
2005-20062005-2006
1
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SubjectT
PC
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05364M
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MATIC
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05433O
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II Year
I Sem
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2005-20062005-2006
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SubjectT
PC
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2005-20062005-2006
3
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DT
P C
I Year B
.Tech
. AE
2+1 0 4(H
S 05231) E
NG
LIS
H1.
INT
RO
DU
CT
ION
:
In view of the grow
ing importance of E
nglish as a tool for global comm
unicationand the consequent em
phasis on training students to acquire comm
unicativeco
mp
ete
nce
, the
syllab
us h
as b
ee
n d
esig
ne
d to
de
velo
p lin
gu
istic an
dcom
municative com
petence of Engineering students. T
he prescribed booksand the exercises are m
eant to serve broadly as students’ handbooks, toencourage them
to develop their language skills. The tw
o textbooks identifiedby the B
oard of Studies serve the purpose of illustrating the conceptual
framew
ork within w
hich the syllabus is to be administered in the classroom
.W
hen a textbook is prescribed content is generally paid attention to. How
ever,the stress in this syllabus is on language acquisition and skill developm
ent,calling for both the teacher and the taught to go beyond the prescribed textsand innovate exercises and tasks.
2.O
BJE
CT
IVE
S :
1.T
o promote the language proficiency of the students w
ith emphasis on im
provingtheir LS
RW
skills.
2.T
o impart training to the students through the syllabus and its theoretical and
practical components.
3.T
o improve com
munication skills in form
al and informal situations.
3.S
YL
LA
BU
S :
Listen
ing
Skills :
•Listening for general content
•Listening to fill up inform
ation gaps•
Intensive listening•
Listening for specific information
•N
ote-taking - guided and unguided•
Post-listening testing
Sp
eaking
Skills :
•O
ral practice•
Developing confidence
•Introducing oneself/others
•A
sking for/ giving information
•D
escribing objects/offering solutions•
Describing situations
•R
ole play•
Expressing agreem
ent/disagreement
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
B.T
EC
H. A
ER
ON
AU
TIC
AL
EN
GIN
EE
RIN
GC
OU
RS
E S
TR
UC
TU
RE
IV Y
earIIn
d S
emester
Co
de
Su
bject
TP
C
AE
05030A
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RA
FT SY
STE
MS
AN
D IN
STR
UM
EN
TS4+1*
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ELECTIVE – III
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E05540
SY
STE
M M
OD
ELIN
G A
ND
SIM
ULATIO
N-
--
AE
05156C
RY
OG
EN
ICS
--
-E
E05404
MIC
RO
PR
OC
ES
SO
RS
& M
ICR
OC
ON
TRO
LER
S-
--
AE
05299H
YP
ER
SO
NIC
AE
RO
DY
NA
MIC
S-
--
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05524SPA
CE
ME
CH
AN
ICS
--
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TIVE – IV4+1*
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AC
TUR
E M
EC
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S-
--
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05102B
OU
ND
AR
Y LAY
ER
THE
OR
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AN
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EM
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--
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05019A
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OE
LAS
TICITY
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A05315
IND
US
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TED
MIN
I PR
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--
2C
A05515
SE
MIN
AR
--
2C
A05495
PR
OJE
CT W
OR
K0
012
TO
TA
L15
028
No
te:T
= Th
eory;
P = P
ractical;* = T
uto
rial;C
= Cred
its
NO
TE
:
1)A
ll bold faced subject syllabi are drafted by Aero E
ngineeringboard m
embers as per the guidelines of JN
TU
.2)
Wherever there are 3 text books they are needed to ensure that
at atleast one cheap book is included. Hence good text books
shouldn’t be omitted for text book recom
mendations.
3)F
urther the multidisciplinary nature of the A
ero Engineering
depends atleast 3 text books per subject.
2005-20062005-2006
4
Read
ing
Co
mp
rehen
sion
•S
kimm
ing the text•
Understanding the gist of an argum
ent•
Identifying the topic sentence•
Inferring lexical and contextual meaning
•U
nderstanding discourse features•
Recognizing coherence/sequencing of sentences
NO
TE
:T
he stu
den
t, thro
ug
h th
e trainin
g im
parted
to h
im/h
er by m
eans
of th
e text-based
app
roach
, will b
e examin
ed in
answ
ering
qu
estion
so
n an
un
seen p
assage.
Writin
g S
kills :•
Writing a sentence
•U
se of appropriate vocabulary•
Paragraph w
riting•
Coherence and cohesiveness
•N
arration / description•
Interpreting data•
Form
al and informal letter w
riting•
Sending e-m
ails•
Information transfer
•E
diting a passage4.
TE
XT
BO
OK
S P
RE
SC
RIB
ED
:In order to im
prove the proficiency of the student in the acquisition of the fourskills m
entioned above, the following texts and course content, divided into
Eight U
nits, are prescribed:1.
LE
AR
NIN
G E
NG
LIS
H: A
Com
municative A
pproach, Hyderabad: O
rientLongm
an, 2005.(Selected Lessons)
2.W
ING
S O
F F
IRE
: An A
utobiography – AP
J Abdul K
alam, A
bridged versionw
ith Exercises, H
yderabad: Universities P
ress (India) Pvt. Ltd., 2004.
Th
e follo
win
g lesso
ns fro
m th
e prescrib
ed texts are reco
mm
end
ed fo
r stud
y :A
.S
TU
DY
MA
TE
RIA
L :
Un
it – I1.
Astro
no
my from
LE
AR
NIN
G E
NG
LIS
H: A
Co
mm
un
icative Ap
pro
ach, O
rientLongm
an, 2005.2.
Chapters 1-4 fro
m W
ings of Fire: A
n Autobiography – A
PJ A
bd
ul K
alam, an
abrid
ged
version
with
Exercises, U
niversities P
ress (Ind
ia) Pvt. L
td., 2004
Un
it – II3.
Info
rma
tion
Te
chn
olo
gy fro
m L
EA
RN
ING
EN
GL
ISH
: A C
omm
unicativeA
pproach, Orien
t Lo
ng
man
, 2005.4.
Chapters 5-8 fro
m W
ings of Fire: A
n Autobiography – A
PJ A
bd
ul K
alam, an
abrid
ged
version
with
Exercises, U
niversities P
ress (Ind
ia) Pvt. L
td., 2004
Un
it – III5.
Hum
our from
LEA
RN
ING
EN
GLIS
H: A
Com
municative A
pproach, Orien
tL
on
gm
an, 2005.
6.C
hapters 9-12 from
Wings of F
ire: An A
utobiography – AP
J Ab
du
l Kalam
, anab
ridg
ed versio
n w
ith E
xercises., Un
iversities Press (In
dia) P
vt. Ltd
., 2004U
nit – IV
7.E
nvironment fro
m LE
AR
NIN
G E
NG
LISH
: A C
omm
unicative Approach, O
rient
Lo
ng
man
, 2005.8.
Chapters 13-16 fro
m W
ings of Fire: A
n Autobiography – A
PJ A
bd
ul K
alam,
an ab
ridg
ed versio
n w
ith E
xercises, Un
iversities Press (In
dia) P
vt. Ltd
.,2004
Un
it – V9.
Inspiration from
LEA
RN
ING
EN
GLIS
H: A
Com
municative A
pproach, Orien
tL
on
gm
an, 2005.
10.C
hapters 17-20 from
Wings of F
ire: An A
utobiography – AP
J Ab
du
l Kalam
,an
abrid
ged
version
with
Exercises, U
niversities P
ress (Ind
ia) Pvt. L
td.,
2004.U
nit – V
I11.
Hum
an Interest from
LEA
RN
ING
EN
GLIS
H : A
Com
municative A
pproach,O
rient L
on
gm
an, 2005.
12.C
hapters 21-24 from
Wings of F
ire: An A
utobiography – AP
J Ab
du
l Kalam
,an
abrid
ged
version
with
Exercises, U
niversities P
ress (Ind
ia) Pvt. L
td.,
2004.* E
xercises from the lessons not prescribed shall also be used for classroom
tasks.U
nit – V
IIR
eading and Writing S
killsR
eading Com
prehensionS
ituational dialoguesR
eport writing
Letter writing
Essay w
ritingInform
ation transferU
nit – V
IIIR
emedial E
nglishC
omm
on errorsS
ubject-Verb agreem
entU
se of Articles and P
repositionsT
ense and aspect
2005-20062005-2006
5
Vo
cabu
lary – Syn
on
yms &
An
ton
yms, o
ne-w
ord
sub
stitutes, p
refixes &su
ffixes, Idio
ms &
ph
rases, wo
rds o
ften co
nfu
sed.
Bo
oks R
ecom
men
ded
:1.
Effective T
echn
ical Co
mm
un
ication
, M A
shraf Rizvi, T
ata McG
raw-H
illP
ublishing Com
pany Ltd.2.
Everyd
ay Dialo
gu
es in E
ng
lish, R
obert J Dixson, P
rentice Hall of India P
vtLtd., N
ew D
elhi.3.
Stren
gth
en Y
ou
r En
glish
, Bhaskaran &
Horsburgh, O
xford University P
ress4.
En
glish
for T
echn
ical Co
mm
un
ication
, K R
Lakshminarayana, S
CIT
EC
H5.
Strateg
ies for E
ng
ineerin
g C
om
mu
nicatio
n, S
usan Stevenson &
Steve
Whitm
ore ( John Wiley and sons).
6.E
ng
lish fo
r En
gin
eers: With
CD
, Sirish C
haudhary, Vikas P
ublishing House
Pvt. Ltd. W
ith CD
.7.
Basic C
om
mu
nicatio
n S
kills for T
echn
olo
gy, A
ndrea J Rutherfoord, P
earsonE
ducation Asia.
8.M
urp
hy’s E
ng
lish G
ramm
ar with
CD
, Murphy, C
ambridge U
niversity Press
9.A
Practical C
ou
rse in E
ng
lish P
ron
un
ciation
, (with
two
Au
dio
cassettes),S
ethi, Sadanand &
Jindal , Prentice –H
all of India Pvt Ltd., N
ew D
elhi.10.
En
glish
for P
rofessio
nal S
tud
ents, by S
S P
rabhakara Rao.
11.T
he O
xford
Gu
ide to
Writin
g an
d S
peakin
g, John S
eely, Oxford.
12.G
ramm
ar Gam
es, Renvolucri M
ario, Cam
bridge University P
ress.
I Year B
.Tech
. AE
T P
C3+1 0 6
(MA
05363) MA
TH
EM
AT
ICS
– IU
NIT
– I
Sequences – series – C
onvergences and divergence – Ratio test – C
omparison
test – Integral test – Cauchy’s root test – R
aabe’s test – Absolute and conditional
convergence. Rolle’s theorem
– Lagrange’s Mean V
alue Theorem
– Cauchy’s M
eanvalue T
heorem – G
eneralized Mean V
alue theorem (T
aylor’s Theorem
).
UN
IT – II
Functions of several variables – F
unctional dependence- Jacobian- Maxim
a andM
inima of functions of tw
o variables with constraints or w
ithout constraints- Radius,
Centre and C
ircle of Curvature – E
volutes and Envelopes.
UN
IT – III
Curve tracing – C
artesian , polar and Param
etric curves - Applications of integration
to lengths , volumes and surface areas in C
artesian and polar coordinates.
UN
IT – IV
Differential equations of first order and first degree – exact, linear and B
ernoulli.A
pplications to New
ton’s Law of cooling, Law
of natural growth and decay, O
rthogonaltrajectories-N
on-homogeneous linear differential equations of second and higher
order with constant coefficients w
ith RH
S term
of the type eax, S
in ax, cos ax,polynom
ials in x, eaxV
(x), xV(x), m
ethod of variation of parameters.
UN
IT – V
Laplace transform of standard functions – Inverse transform
– first shifting Theorem
,T
ransforms of derivatives and integrals – U
nit step function – second shifting theorem– D
irac’s delta function – Convolution theorem
– Periodic function - D
ifferentiationand integration of transform
s-Application of Laplace transform
s to ordinary differentialequations.
UN
IT – V
I
Multiple integrals - double and triple integrals – change of variables – change of
order of integration.
UN
IT – V
II
Vector C
alculus: Gradient- D
ivergence- Curl and their related properties of sum
s-products- Laplacian and second order operators. V
ector Integration - Line integral– w
ork done – Potential function – area- surface and volum
e integrals.
UN
IT – V
III
Vector integral theorem
s: Green’s theorem
- Stoke’s and G
auss’s Divergence
Theorem
. Verification of G
reen’s - Stoke’s and G
auss’s Theorem
s – Cylindrical,
Spherical coordinates-E
xpressions Grad, div, curl in spherical and cylindrical
coordinates.
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
2005-20062005-2006
6
TE
XT
BO
OK
S :
1.A
text book of Engineering M
athematics V
olume – 1, 2005
T.K
.V.Iyengar, B
.Krishna G
andhi and others, S.C
hand and Com
pany.
2.E
ngineering Mathem
atics, B.V
.Ram
ana, Tata M
cGraw
-Hill 2003.
RE
FE
RE
NC
ES
:
1.E
ng
ine
erin
g M
ath
em
atics–
I, 20
02
, P.N
ag
esw
ara
Ra
o, Y
.Na
rsimh
ulu
,P
rabhakara Rao, D
eepthi Publishers
2.E
ngineering Mathem
atics- I, 2004, Dr.S
hahnaz Bathul, R
ight Publishers.
3.E
ngineering Mathem
atics, S.K
.V.S
. Sri R
ama C
hary, M.B
hujanga Rao,
Shankar, B
.S. P
ublications 2000.
4.E
ngineering Mathem
atics-I Rukm
angadhachary, Pearson E
ducation.
5.A
Text book of E
ngineering Mathem
atics, VP
Mishra, G
algotia Publications.
6.E
ngineering Mathem
atics – I, Sankaraiah, V
GS
Book Links, H
yderabad.
I year B.T
ech A
.E.
T P
C 2+1 0 4
(PY
05226) EN
GIN
EE
RIN
G P
HY
SIC
S
UN
IT – I
INT
ER
FE
RE
NC
E Introduction - S
uperposition of waves - Y
oung’s double slitexperim
ent - Coherence - Interference in thin film
s by reflection - New
ton’s rings.
DIF
FR
AC
TIO
N Introduction - F
ressnel and Fraunhofer diffraction - F
raunhoferdiffraction at a single slit &
at a double slit - Circular aperture - D
iffraction grating -
Grating spectrum
- Resolving pow
er of a grating - Rayleigh’s criterion for resolving
power.
UN
IT II
PO
LA
RIZ
AT
ION
Introduction - Representation of polarized and unpolarized light -
Polarization by reflection - M
alus law - D
ouble refraction - Nicol prism
- Circular and
Elliptical polarization -Q
uarter wave plate - H
alf wave plate.
UL
TR
AS
ON
ICS
Introduction - Production of U
ltrasonic waves - M
agnetostriction
method - P
iezo electric method - D
etection of Ultrasonics - P
roperties of Ultrasonics
- Use of U
ltrasonics for non-destructive testing - Applications of U
ltrasonics.
UN
IT III
AC
OU
ST
ICS
OF
BU
ILD
ING
S B
asic re
qu
irem
en
t of a
cou
stically g
oo
d h
all -
Reverberation and tim
e of reverberation – Sabine’s form
ula for reverberation time -
Me
asu
rem
en
t of a
bso
rptio
n co
efficie
nt o
f a m
ate
rial - F
acto
rs affe
cting
the
architectural acoustics and their remedy.
SU
PE
RC
ON
DU
CT
IVIT
Y G
eneral properties - Meissner effect - P
enetration depth -
Type I and T
ype II superconductors - Flux quantization - Josephson E
ffect - BC
S
Theory - A
pplications of superconductors.
UN
IT IV
LA
SE
RS
Introduction - Characteristics of Lasers - S
pontaneous and Stim
ulated
Em
ission of radiation - Einstein’s coefficients - P
opulation inversion - Ruby Laser -
Helium
-Neon Laser - S
emiconductor Laser - A
pplications of Lasers in Industry,S
cientific and Medical fields.
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
2005-20062005-2006
7
UN
IT V
FIB
ER
OP
TIC
S Introduction - P
rinciple of optical fiber - Acceptance angle and
Acceptance cone - N
umerical aperture - S
tep-Index fiber and transmission of signal
in SI fiber - G
raded-Index fiber and transmission of signal in G
I fiber - Attenuation in
optical fibers - Advantages of optical fibers in com
munication - A
pplication of opticalfibers in M
edicine and Sensors.
UN
IT V
IM
AG
NE
TIC
PR
OP
ER
TIE
S P
ermeability - M
agnetization - Origin of m
agnetic mom
ent- C
lassification of magnetic m
aterials - Dia, P
ara and Ferro m
agnetism - H
ysteresiscurve - S
oft and Hard m
agnetic materials - anti-F
erro and Ferri m
agnetism - F
erritesand their applications.C
RY
ST
AL
ST
RU
CT
UR
ES
Introduction - Space lattice - B
asis - Unit cell - Lattice
parameter - C
rystal systems - B
ravais lattices - Structure and P
acking fractions ofS
imple cubic - B
ody Centred C
ubic - Face C
entred Cubic crystals - S
tructures ofD
iamond, Z
nS, N
aCl, C
sCl.
UN
IT V
IIC
RY
ST
AL
PL
AN
ES
& X
-RA
Y D
IFF
RA
CT
ION
Directions and P
lanes in crystals -M
iller Indices - Separation betw
een successive [h k l] planes - Diffraction of X
-raysby C
rystal planes - Bragg’s Law
- Laue method -P
owder m
ethod.
UN
IT V
IIID
EF
EC
TS
IN S
OL
IDS
Imperfections in C
rystals - Point defects - S
chottky and Frenkel
defects - Energy for form
ation of a Vacancy - E
quilibrium concentration of S
chottkyand F
renkel defects -Line defects - Edge and S
crew dislocation - B
urger’s Vectors.
Text B
oo
ks:1.
En
gin
eering
Ph
ysics by R.K
.Gaur - S
.L. Gupta; D
hanpat Rai and S
ons.2.
Ap
plied
Ph
ysics by Dr. M
.Chandra S
hekar & D
r.P.A
ppala Naidu; V
.G.S
. Book
links.
Referen
ces :1.
En
gin
eering
Ph
ysics by Dr.M
. Arum
ugam; A
nuradha Agencies
2.P
hysics V
olu
me 2, by H
alliday, Resnick and K
rane; John Wiley &
Sons
3.E
ng
ineerin
g P
hysics by M
.N.A
vadhanulu & P
.G. K
shirasagar; S.C
hand&
Com
pany Ltd.4.
En
gin
eering
Ph
ysics by P.V
.Naik; P
earson Education
5.M
aterials Scien
ce and
En
gin
eering
by V. R
aghavan; Prentice-H
all India6.
En
gin
eering
Ph
ysics (Vo
l.1) by M.D
. Khanna and V
. Balasw
amy; V
ikasP
ublishing House P
vt. Ltd., New
Delhi
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
I Year B
. Tech
. AE
T P
C3+1 0 6
(ME
05224) EN
GIN
EE
RIN
G M
EC
HA
NIC
S
UN
IT – I7
Introduction to Engg. M
echanics – Basic C
onceptsS
ystems of F
orces :C
oplanar Concurrent F
orces – Com
ponents in Space – R
esultant – Mom
ent ofF
orce and its Application – C
ouples and Resultant of F
orce System
s.E
quilibrium of S
ystems of F
orces :F
ree Body D
iagrams, E
quations of Equilibrium
of Coplanar S
ystems, S
patial System
sfor concurrent forces.
UN
IT – II
Friction : T
ypes of Friction – Lim
iting Friction – Law
s of Friction – S
tatic and Dynam
icF
rictions – Motion of B
odies: Wedge, S
crew, S
crew-jack, and D
ifferential Screw
-jack.
UN
IT – III
Transm
ission of Pow
er : Flat B
elt Drives : T
ypes of Flat B
elt Drives – Length of B
elt,T
ensions, Tight side, S
lack Side, Initial and C
entrifugal – Pow
er Transm
itted andC
ondition for Max. P
ower.
UN
IT – IV
Centroid: C
entroids of simple figures (from
basic principles ) – Centroids of C
omposite
Figures
Centre of G
ravity: Centre of gravity of sim
ple body (from basis principles), centre of
gravity of composite bodies, pappus theorem
.
UN
IT – V
Area m
oments of Inertia : D
efinition – Polar M
oment of Inertia, T
ransfer Theorem
,M
oments of Inertia of C
omposite F
igures, Products of Inertia, T
ransfer Form
ula forP
roduct of Inertia.M
ass Mom
ent of Inertia : Mom
ent of Inertia of Masses, T
ransfer Form
ula for Mass
Mom
ents of Inertia, mass m
oment of inertia of com
posite bodies.
UN
IT – V
IK
inematics : R
ectilinear and Curvelinear m
otions – Velocity and A
cceleration – Motion
of Rigid B
ody – Types and their A
nalysis in Planar M
otion.K
inetics : Analysis as a P
article and Analysis as a R
igid Body in T
ranslation – Central
Force M
otion – Equations of P
lane Motion – F
ixed Axis R
otation – Rolling B
odies.
2005-20062005-2006
8
UN
IT – V
IIW
ork – Energy M
ethod :E
quations for Translation, W
ork-Energy A
pplications to Particle M
otion, Connected
System
-Fixed A
xis Rotation and P
lane Motion.
Impulse m
omentum
method :
UN
IT – V
IIIM
echanical Vibrations : D
efinitions, Concepts – S
imple H
armonic M
otion – Free
vibrations, simple and C
ompound P
endulums and its A
pplications –
TE
XT
BO
OK
S :
1. Engineering M
echanics / Fedinand . L. S
inger / Harper – C
ollins.2. E
ngg. Mechanics / S
.S. B
havikati & J.G
. Rajasekharappa
RE
FE
RE
NC
E :
1.E
ngg. Mechanics / Irving. H
. Sham
es Prentice – H
all.2.
Engg. M
echanics / Tim
oshenko & Y
ound.3.
Engg. M
echanics Um
esh Regl / T
ayal.4.
Engg. M
echanics / R.V
. Kulkarni &
R.D
. Askhevkar
5.S
trength of Materials &
Applied M
echanics / IB P
rasad6.
Text B
ook in Applied M
echanics / Malhotra, S
ubramanian,
Gahlot and R
athore / New
Age.
7.E
ngg. Mechanics / K
L Kum
ar / Tata M
cGraw
Hill.
8.E
ngg. Mechanics / R
ajasekharan
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DI Y
ear B. T
ech. A
ET
P C
3+1 0 6(M
A05431) N
UM
ER
ICA
L M
ET
HO
DS
UN
IT-IS
olutions of Algebraic and Transcendental E
quations: Introduction-The Bisection M
ethod-The m
ethod of False Position- The Iteration M
ethod- New
ton-Raphson M
ethod.U
NIT-II
Interpolation: Introduction –Errors in polynom
ial Interpolation- Finite differences – Forward
Differences- B
ackward differences –S
ymbolic relations and separation of sym
bols- Differences
of a polynomial –N
ewton’s form
ulae for Interpolation- central difference Interpolation formulae-
Gauss central D
ifference Formulae- Interpolation w
ith unevenly spaced points- Lagrange’sInterpolation form
ula.
UN
IT-IIIFitting a straight line – N
onlinear curve fitting- curve fitting by a sum of E
xponentials- Weighted
least squares approximation –Linear w
eighted least squares approximation- N
onlinearw
eighted least square.U
NIT-IV
Orthogonal polynom
ials-Gram
s Schm
idt orthogonalization process- Least-square solution-R
epresentation of B-splines- C
omputation of B
-splines- The Fourier Transform-The Fast Fourier
transform.
UN
IT-VN
umerical D
ifferentiation and Integration: The cubic Spline m
ethod- Trapezoidal rule –S
impson’s one-third rule- S
impson’s 3/8 rule – B
oole’s and Weddle’s R
ules.
UN
IT-VIM
atrices and linear systems of E
quations: Solution of Linear S
ystems- D
irect Methods –LU
Decom
position- LU D
ecomposition from
Gauss E
limination – S
olution of Tridiagonal System
s– S
olution of Linear System
s.U
NIT-VII
Num
erical Solutions of ordinary D
ifferential Equations: S
olutions by Taylor’s Series –P
icard’sM
ethod of successive Approxim
ations – Euler’s m
ethod- Runge-K
utta Methods- P
redictor –C
orrector Methods – A
dams M
oulton Method – M
ilne’s Method.
UN
IT-VIIIN
umerical S
olutions of Partial D
ifferential Equations: Introduction- Finite D
ifferenceA
pproximations to D
erivatives –Laplace’s Equation –Jacobi’s M
ethod – Gauss-S
eidel Method.
TEXT BO
OK
S1.
Introductory methods of N
umerical A
nalysis: S.S
. Sastry, P
rentice Hall of India, P
vt. Ltd.2.
Num
erical Methods: Jain, Iyengar.
REFER
ENC
ES1.
Num
erical Methods: V.N
. Vedamurthy, Iyengar N
, Ch N
Vikas P
ub. Reprint 2005.
2.N
umerical M
ethods: S. A
rumugam
& others, S
ciTech Pub.
3.E
lementary N
umerical A
nalysis: An A
lgorithm A
pproach: S.D
. Conte and C
arl. D.E
.B
oor, Tata Mc-G
raw H
ill.
2005-20062005-2006
9
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
I Year B
.Tech
. AE
.T
P C
3 0 6
(CS
05106) C P
RO
GR
AM
MIN
G A
ND
DA
TA
ST
RU
CT
UR
ES
UN
IT - I
Algorithm
, flowchart, program
development steps, basic structures of C
language,
C tokens, data types and sizes, declaration of variables, assigning values, arith-
metic, relational and logical operator, increm
ent and decrement operators, condi-
tional operator, bit-wise operators, type conversions, expressions, evaluation, in-
put-output statements, blocks, if and sw
itch statement, w
hile, do-while and for state-
ments, C
programs covering all the above aspects.
UN
IT - II
One dim
ensional & T
wo dim
ensional arrays, initialization, string variables-declara-
tion, reading, writing, B
asics of functions,Param
eter pasing,String handling func-
tion, user-defined functions, recursive functions, variables and storage classes, scope
rules, block structure, header files, C preprocessor, exam
ple C program
s.
UN
IT - III
Po
inter an
d A
rrays : Pointers and addresses, P
ointers and Arrays, P
ointers And
function arguments, A
ddress arithmetic, character pointers and functions, pointers
to pointers, multi-dim
ensional arrays, initialization of pointer arrays, comm
and line
arguments, pointers to functions.
UN
IT - IV
Stru
ctures : D
efinition, initializing, assigning values, passing of structures as ar-
guments, A
rrays of structures, pointers to structures, self referential structures.
Unions, typedef, bit fields, C
program exam
ples.
UN
IT - V
Co
nso
le & F
ile I/O : S
tandard I/O, F
ormatted I/O
, opening & closing of files, I/O
operations on files.
UN
IT - V
I
Lin
ear DataS
tructu
res : Introduction to DataS
tructures, representing stacks and
queues in C using arrays, Infix, P
ostfix & P
refix programs, circular queues.
UN
IT - V
II
Lin
ked L
ists : Singly linked list, D
oubly linked list, Circular List, representing stacks
and Queues in C
using linked lists
No
n-L
inear D
ata Stru
ctures : B
inary trees: Representation, tree traversals, graph
representation, graph traversal, Spanning trees.
UN
IT - V
III
So
rting
& S
earchin
g : S
earching Methods- Linear and binary search m
ethods,
Sorting m
ethods- Ex: B
ubble sort, Selection sort, Insertion sort, heap sort, quick
sort.
TE
XT
BO
OK
S :
1.C
and Data structures – P
.Padm
anabham, B
S P
ublications
2.C
& D
ata Structures, A
shok N.K
amthane, P
earson Education
RE
FE
RE
NC
ES
:
1.C
& D
ata
Stru
cture
s – P
rof. P
.S.D
esh
Pa
nd
e, P
rof O
.G.K
akd
e, W
iley
Dream
tech Pvt. Ltd., N
ewD
elhi.
2.D
ataStructures U
sing C – A
.S.T
anenbaum, P
HI/P
earson education
3.T
he C P
rogramm
ing Language, B.W
. Kernighan, D
ennis M.R
itchie, PH
I/
Pearson E
ducation
2005-20062005-2006
10
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
I Year B
. Tech
. AE
T P
C0 – 6 – 8
(ME
05223) EN
GIN
EE
RIN
G G
RA
PH
ICS
UN
IT – I
INT
RO
DU
CT
ION
TO
EN
GIN
EE
RIN
G D
RA
WIN
G :
Principles of E
ngineering Graphics and their S
ignificance – Draw
ing Instruments
and their Use – C
onventions in Draw
ing – Lettering – BIS
Conventions.
Scales used in E
ngineering Practice and R
epresentative Fraction – C
onstruction ofP
lain, Diagonal and V
ernier Scales.
UN
IT – II
PL
AN
E G
EO
ME
TR
IC D
RA
WIN
G :
Construction of P
olygons – Inscription and Superscription of P
olygon given thediam
eter of the Circles.
Curves used in E
ngineering Practice and their C
onstructionsa)
Conic S
ections including the Rectangular H
yperbola – General m
ethod only.b)
Cycloid, E
picycloid and Hypocycloid
c)Involute.
UN
IT – III
DR
AW
ING
OF
PR
OJE
CT
ION
S O
R V
IEW
SO
RT
HO
GR
AP
HIC
PR
OJE
CT
ION
IN F
IRS
T A
NG
LE
PR
OJE
CT
ION
ON
LY
:P
rinciples of Orthographic P
rojections – Conventions – F
irst and Third A
ngleP
rojections Projections of P
oints and Lines inclined to both planes, True lengths,
traces -P
rojections of Planes regular auxiliary planes and A
uxiliary projection inclined toboth planes.
UN
IT – IV
PR
OJE
CT
ION
S O
F S
OL
IDS
Projections of R
egular Solids inclined to both planes – A
uxiliary View
s.S
ections and Sectional view
s of Right R
egular Solids – P
rism, C
ylinder, Pyram
id,C
one – Auxiliary view
s.
UN
IT – V
DE
VE
LO
PM
EN
T A
ND
INT
ER
PE
NE
TR
AT
ION
OF
SO
LID
S
Developm
ent of Surfaces of R
ight Regular S
olids – Prism
s, Cylinder, P
yramid C
oneand their parts.Interpenetration of R
ight Regular S
olids – Intersection of Cylinder V
s Cylinder, C
ylinderV
s Prism
, Cylinder V
s Cone.
UN
IT – V
I
ISO
ME
TR
IC P
OR
JEC
TIO
NS
:P
rinciples of Isometric P
rojection – Isometric S
cale – Isometric V
iews – C
onventions– Isom
etric View
s of Lines, Plane F
igures, Sim
ple and Com
pound Solids – Isom
etricP
rojection of objects having non- isometric lines. Isom
etric Projection of S
phericalP
arts.
UN
IT –V
II
TR
AN
SF
OR
MA
TIO
N O
F P
RO
JEC
TIO
NS
:C
onversion of Isometric V
iews to O
rthographic View
s – Conventions :
UN
IT – V
III
PE
RS
PE
CT
IVE
PR
OJE
CT
ION
S :
Perspective V
iew : P
oints, Lines, Plane F
igures and Sim
ple Solids ,V
anishing Point
Methods(G
eneral Method only)
TE
XT
BO
OK
:1.
Engineering D
rawing, N
.D. B
hat / Charotar
Referen
ces:1.
Engineering D
rawing, N
arayana and Kannaiah / S
cietech publishers.2.
Engineering D
rawing and G
raphics, Venugopal / N
ew age.
2005-20062005-2006
11
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
I Year B
. Tech
. AE
T P
C0 – 3 – 4
(CS
05144) CO
MP
UT
ER
PR
OG
RA
MM
ING
LA
B
1.W
rite a C program
the evaluates the following algebraic expressions after
reading necessary values from the user:
a)ax+
b/ax-bb)
2.5 log x + cos 32
0 + | x2 –y
2 | + √ √ √ √ √ 2xy
c)1/α √√ √√√
2 π e- (x-m
/ √√ √√√2 σ) 2
2.W
rite a C program
for the following
a)P
rinting three given integers in ascending orderb)
Sum
of 1 + 2+ 3 + _ _ _ _ _ nc)
1 + x2/2! + x
2/ 4!+ _ _ _ _ _ upto ten terms
d)x +x
3/3! + x5/5!+ _ _ _ _ _ upto 7
th digit accuracye)
Read x and com
pute Y =1 for x > 0
Y=0 for x = 0
Y= -1 for x<0
3.W
rite C program
using FO
R statem
ent to find the following from
a given set of20 integers.i) T
otal number of even integers. ii) T
otal number of odd integers.
iii) Sum
of all even integers. iv) Sum
of all odd integers.
4.W
rite a C program
to obtain the product of two m
atrices A of size (3X
3) andB
of size (3X2). T
he resultant matrix C
is to be printed out along with A
andB
. Assum
e suitable values for A &
B.
5.U
sing switch-case statem
ent, write a C
program that takes tw
o operands andone operator from
the user, performs the operation and then prints the answ
er.(consider operators +
,-,/,* and %).
6.W
rite C procedures to add, subtract, m
ultiply and divide two com
plex numbers
(x+iy) and (a+
ib). Also w
rite the main program
that uses these procedures.
7.T
he total distance traveled by vehicle in ‘t’ seconds is given by distance =ut+1/2at 2 w
here ‘u’ and ‘a’ are the initial velocity (m/sec.) and acceleration (m
/sec
2). Write C
program to find the distance traveled at regular intervals of tim
egiven the values of ‘u’ and ‘a’. T
he program should provide the flexibility to the
user to select his own tim
e intervals and repeat the calculations for differentvalues of ‘u’ and ‘a’.
Purchase A
mount
Discount (P
ercentage)
Mill C
lothH
andloom item
s
1-100-
5.0
101-2005.0
7.5
201-3007.5
10.0
Above 300
10.015.0
8.A
cloth show room
has announced the following seasonal discounts on
purchase of items.
Write a C
program using sw
itch and If statements to com
plete the net amount
to be paid by a customer.
9.G
iven a number, w
rite C program
using while loop to reverse the digits of the
number. E
xample 1234 to be w
ritten as 4321.10.
The F
ibonacci sequence of numbers is 1,1,2,3,5,8…
based on therecurrence relationf(n) =
f (n-1) + f (n-2) for n>
2.W
rite C program
using d0-while to calculate and print the first m
fibonaccinum
bers.11.
Write C
programs to print the follow
ing outputs using for loop.
12.W
rite a C program
to extract a portion of a character string and print theextracted string. A
ssume that m
characters are extracted starting with the nth
character.
13.A
Maruthi C
ar dealer maintains a record of sales of various vehicles in the
following form
:
122
33
34
44
45
55
55
12
23
33
44
44
55
55
5
Veh
icle type
Mo
nth
of S
alesP
rice (Rs).
Maruthi – 800
02/8775,000
Maruthi – D
X07/87
95,000
Gypsy
04/881,10,000
Maruthi V
an08/88
85,000
Write a C
program to read this data into a table of strings and output the
details of a particular vehicle sold during a specified period. The program
should request the user to input the vehicle type and the period (Starting m
onth&
ending month).
2005-20062005-2006
12
14.W
rite a function that will scan a character string passed as an argum
ent andcovert all low
er case characters into their upper case equivalents.
15.Im
plement the follow
ing data structures using Arrays
i) Stacks ii) Linear Q
ueues iii) Circular queues iv) D
equeue.
16.Im
plement polynom
ial addition and multiplication w
ith linked list sparse matrix.
17.Im
plement binary search tree using linked list and perform
the following
operations.i) Insertion
ii) Deletion iii) Inorder T
raversaliv) P
reorder Traversal
v) Post O
rder Traversal.
18.S
ingly linked list and doubly linked listsi) Insertion
ii) Deletion
iii) Lookup
19.i) Im
plement stack using singly linked list.
ii) Implem
ent queue using singly linked list.
20.Im
plement the follow
ing sorting techniques.i) B
ubble sortii) Insertion S
ortiii) Q
uick Sort
iv) Heap S
ort.
21.Im
plement the follow
ing searching method.
i) Sequential S
earchii) B
inary Search
iii) Fibonacci
22.i) C
onversion of Infix expression to Postfix notation.
ii) Sim
ple expression evaluator, that can handle +,-,/ and *.
23.Im
plement the algorithm
s for the following iterative m
ethods using C to find
one root of the equation9x
1 +2x2 +4x
3 = 0x
1 +10x2 +4x
3 = 62x
1 -4x2 +10x
3 = -15.
25.W
rite Com
puter programs to im
plement the Lagrange interpolation and N
ewton-
Gregory forw
ard interpolation.
26.Im
plement in ‘C
’ the linear regression and polynomial regression algorithm
s.
27.Im
plement T
raezoidal and Sim
pson methods.
28.P
ractice of exercises (in text book 2 of theory) related to:a) W
ord 2000 Chapter 7, 8, 9.
b) Excel 2000 C
hapter 12, 13.c) P
owerpoint- 2000 C
hapter 15, 16.d) A
ccess 2000 Chapter 18,19.
e) Outlook 2000 C
hapter 21,22,23.f) F
rontPage 2000 C
hapter 25
JAWAHARLAL NEHRU TECHNO
LOG
ICAL UNIVERSITYHYDERABAD
I Year B.Tech. AET P C0 3 4
(CS 05337) IT WO
RKSHOP
Objectives :
The IT Workshop for engineers is a 6 training lab course spread over 90 hours. The m
odules includetraining on PC
Hardw
are, Internet & World W
ide Web and Productivity tools including M
S Word,
Excel, Power Point and Publisher.
PC Hardware introduces the students to a personal com
puter and its basic peripherals, the processof assem
bling a personal computer, installation of system
software like W
indows XP, Linux and the
required device drivers. In addition hardware and softw
are level troubleshooting process, tips andtricks w
ould be covered.
Internet & World W
ide Web m
odule introduces the different ways of hooking the PC
on to the internetfrom
home and w
orkplace and effectively usage of the internet. Usage of w
eb browsers, em
ail,new
sgroups and discussion forums w
ould be covered. In addition, awareness of cyber hygiene, i.e.,
protecting the personal computer from
getting infected with the viruses, w
orms and other cyber attacks
would be introduced.
Productivity tools module w
ould enable the students in crafting professional word docum
ents, excelspread sheets, pow
er point presentations and personal web sites using the M
icrosoft suite of officetools and LaTeX.
PC Hardware
Week 1 – Task 1 : Identify the peripherals of a com
puter, components in a C
PU and its functions.
Draw
the block diagram of the C
PU along w
ith the configuration of each peripheral and submit to your
instructor.
Week 2 – Task 2 : Every student should disassem
ble and assemble the PC
back to working condition.
Lab instructors should verify the work and follow
it up with a Viva. Also students need to go through
the video which show
s the process of assembling a PC
. A video would be given as part of the course
content.
Week 3 – Task 3 : Every student should individually install w
indows XP on the personal com
puter.Lab instructor should verify the installation and follow
it up with a Viva.
Week 4 – Task 4 : Every student should install Linux on the com
puter. This computer should have
window
s installed. The system should be configured as dual boot w
ith both window
s and Linux. Labinstructors should verify the installation and follow
it up with a Viva
Week 5 – Task 5 : Several m
ini tasks would be that covers Basic com
mands in Linux and Basic
system adm
inistration in Linux which includes: Basic Linux com
mands in bash, C
reate hard andsym
bolic links, Text processing, Using w
ildcards
Week 6 – Task 6 : Hardw
are Troubleshooting : Students have to be given a PC w
hich does notboot due to im
proper assembly or defective peripherals. They should identify the problem
and fix it toget the com
puter back to working condition. The w
ork done should be verified by the instructor andfollow
ed up with a Viva
Week 7 – Task 7 : Softw
are Troubleshooting : Students have to be given a malfunctioning C
PUdue to system
software problem
s. They should identify the problem and fix it to get the com
puter back
2005-20062005-2006
13
to working condition. The w
ork done should be verified by the instructor and followed up w
ith a Viva.
Week 8 – Task 8 : The test consists of various system
s with H
ardware / Softw
are related troubles,Form
atted disks without operating system
s.
Internet & World W
ide Web
Week 9 - Task 1 : O
rientation & Connectivity Boot Camp : Students should get connected to their
Local Area Netw
ork and access the Internet. In the process they configure the TCP/IP setting. Finally
students should demonstrate, to the instructor, how
to access the websites and em
ail. If there is nointernet connectivity preparations need to be m
ade by the instructors to simulate the W
WW
on theLAN
.
Week 10 - Task 2 : W
eb Browsers, Surfing the W
eb : Students customize their w
eb browsers w
iththe LAN
proxy settings, bookmarks, search toolbars and pop up blockers. Also, plug-ins like M
acromedia
Flash and JRE for applets should be configured.
Week 11 - Task 3 : Search Engines & Netiquette : Students should know
what search engines are
and how to use the search engines. A few
topics would be given to the students for w
hich they need tosearch on G
oogle. This should be demonstrated to the instructors.
Week 12 - Task 4 : Cyber Hygiene : Students w
ould be exposed to the various threats on theinternet and w
ould be asked to configure their computer to be safe on the internet. They need to first
install an anti virus software, configure their personal firew
all and window
s update on their computer.
Then they need to customize their brow
sers to block pop ups, block active x downloads to avoid
viruses and/or worm
s.
Week 13 M
odule Test A test which sim
ulates all of the above tasks would be crafted and given to the
students.
LaT
eX an
d M
icroso
ft Wo
rd
Week 14 – W
ord
Orien
tation
: The m
entor needs to give an overview of LaT
eXand M
icrosoft word : Im
portance of LaTeX
and MS
Word as w
ord Processors, D
etailsof the four tasks and features that w
ould be covered in each, Using LaT
eX and w
ord– A
ccessing, overview of toolbars, saving files, U
sing help and resources, rulers,form
at painter in word.
Task 1 : U
sing
LaT
eX an
d w
ord
to create project certificate. Features to be covered:-
Form
atting Fonts in w
ord, Drop C
ap in word, A
pplying Text effects, U
sing Character
Spacing, B
orders and Colors, Inserting H
eader and Footer, U
sing Date and T
ime
option in both LaTeX
and Word.
Week 15 - T
ask 2 : Creatin
g p
roject abstract F
eatures to be covered:-Form
attingS
tyles, Inserting table, Bullets and N
umbering, C
hanging Text D
irection, Cell
alignment, F
ootnote, Hyperlink, S
ymbols, S
pell Check , T
rack Changes.
Week 16 - T
ask 3 : Creatin
g a N
ewsletter : F
eatures to be covered:- Table of
Content, N
ewspaper colum
ns, Images from
files and clipart, Draw
ing toolbar andW
ord Art, F
ormatting Im
ages, Textboxes and P
aragraphs
Week 17 - T
ask 4 : Creatin
g a F
eedb
ack form
- Features to be covered- F
orms,
Text F
ields, Inserting objects, Mail M
erge in Word.
Week 18 - L
aTeX
and
Wo
rd M
od
ule T
est - Replicate the given docum
ent inclusiveof all features
Micro
soft E
xcel
Week 19 - E
xcel Orien
tation
: The m
entor needs to tell the importance of M
SE
xcel as a Spreadsheet tool, give the details of the four tasks and features that
would be covered in each. U
sing Excel – A
ccessing, overview of toolbars, saving
excel files, Using help and resources
Task 1 : C
reating
a Sch
edu
ler - Features to be covered:- G
ridlines, Form
at Cells,
Sum
mation, auto fill, F
ormatting T
ext
Week 20 - T
ask 2 : Calcu
lating
GP
A - .F
eatures to be covered:- Cell R
eferencing,F
ormulae in excel – average, std.deviation, C
harts, Renam
ing and Insertingw
orksheets, Hyper linking, C
ount function, HLO
OK
UP
/VLO
OK
UP
Week 21 - T
ask 3 : Perfo
rman
ce An
alysis - Features to be covered:- S
plit cells,freeze panes, group and outline, S
orting, Boolean and logical operators, C
onditionalform
atting
Week 22 - T
ask 4 : Cricket S
core C
ard - F
eatures to be covered:-Pivot T
ables,Interactive B
uttons, Importing D
ata, Data P
rotection, Data V
alidation,
Week 23 – E
xcel Mo
du
le Test - R
eplicate the given document inclusive of all features
LaT
eX an
d M
icroso
ft Po
wer P
oin
t
Week 24 - T
ask1 : Students w
ill be working on basic pow
er point utilities and toolsw
hich help them create basic pow
er point presentation.
Topic covered during this w
eek includes :- PP
T O
rientation, Slide Layouts, Inserting
Text, W
ord Art, F
ormatting T
ext, Bullets and N
umbering, A
uto Shapes, Lines and
Arrow
s in both LaTeX
and Pow
erpoint.
Week 25 - T
ask 2 : Second w
eek helps students in making their presentations
interactive.
Topic covered during this w
eek includes : Hyperlinks, Inserting –Im
ages, Clip A
rt,A
udio, Video, O
bjects, Tables and C
harts
Week 26 - T
ask 3 : Concentrating on the in and out of M
icrosoft power point and
presentations in LaTeX
. Helps them
learn best practices in designing and preparingpow
er point presentation.
Topic covered during this w
eek includes :- Master Layouts (slide, tem
plate, andnotes), T
ypes of views (basic, presentation, slide slotter, notes etc), Inserting –
Background, textures, D
esign Tem
plates, Hidden slides.
2005-20062005-2006
14
Week 27 - T
ask 4 : Entire w
eek concentrates on presentation part of LaTeX
andM
icrosoft power point.
Topic covered during this w
eek includes -Using A
uto content wizard, S
lide Transition,
Custom
Anim
ation, Auto R
ehearsing
Week 28 - T
ask 5 : Pow
er point test would be conducted. S
tudents will be given
model pow
er point presentation which needs to be replicated (exactly how
it’s asked).
Micro
soft P
ub
lisher
Week 29 : H
elp students in preparing their personal website using M
icrosoftpublisher.
Topic covered during this w
eek includes - Publisher O
rientation, Using T
emplates,
Layouts, Inserting text objects, Editing text objects, Inserting T
ables, Working w
ithm
enu objects, Inserting pages, Hyper linking, R
enaming, deleting, m
odifying pages,H
osting website.
RE
FE
RE
NC
ES
:
1.C
om
de
x Info
rma
tion
Te
chn
olo
gy co
urse
too
l kit ‘Vika
s Gu
pta
, WIL
EY
Dream
tech
2.T
he Com
plete Com
puter upgrade and repair book,3rd edition Cheryl A
Schm
idt, WILE
Y D
reamtech
3.Introduction to Inform
ation Technology, IT
L Education S
olutions limited,
Pearson E
ducation.
4.P
C H
ardware and A
+H
andbook – Kate J. C
hase PH
I (Microsoft)
5.LaT
eX C
ompanion – Leslie Lam
port, PH
I/Pearson.
6.A
ll LaTeX
and others related material is available at
(a)w
ww
.sssolutions.in and
(b)w
ww
.sontisoftsolutions.org
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
I Year B
. Tech
. AE
T P
C0 – 3 – 4
(ME
05230) EN
GIN
EE
RIN
G W
OR
KS
HO
P P
RA
CT
ICE
1. TR
AD
ES
FO
R E
XE
RC
ISE
S:
1.C
arpentry2.
Fitting
3.T
in-Sm
ithy and Developm
ent of jobs carried out and soldering.4.
Black S
mithy
5.H
ouse-wiring
6.F
oundry7.
IT W
orkshop-I : Com
puter hard ware , identification of parts , D
isassembly,
Assem
bly of computer to w
orking condition, Sim
ple diagnostic exercises.8.
IT w
orkshop-II : Installation of Operating system
window
s and Linux , simple
diagnostic exercises.
II TR
AD
ES
FO
R D
EM
ON
ST
RA
TIO
N &
EX
PO
SU
RE
:1.
Plum
bing2.
Welding
3.M
achine Shop
4.P
ower tools in construction, W
ood working, E
lectricalE
ngg & M
echanical Engg
5.M
etal Cutting (w
ater plasma)
Text B
oo
ks: Work shop M
anual / P.K
annaiah/ K.L.N
arayana/ Scitech publishers
2005-20062005-2006
15
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DI Y
ear B. T
ech. A
ET
P C
0 – 3 – 4
(HS05232) EN
GLISH
LAN
GU
AG
E CO
MM
UN
ICATIO
N SK
ILLS LAB
Syllabus
The follow
ing course content is prescribed for the English
Language Laboratory Practice
1.Introduction to P
honetics.2.
Introduction to Vow
els and Consonants and associated P
honetic symbols.
3.Introduction to A
ccent, Intonation and Rhythm
.4.
Situational D
ialogues / Role P
lay.5.
Public S
peaking.6.
Debate
7.G
roup discussions8.
Facing Interview
s9.
Resum
e preparation10.
e-correspondence
Min
imu
m R
equ
iremen
t
�C
omputer aided m
ulti media language lab w
ith 30 systems w
ith LAN
facility.�
Conventional Language Lab. w
ith audio and video systems, speakers,
head phones and a teacher console to accomm
odate 30 students.
Su
gg
ested S
oftw
are:�
Cam
bridge Advanced Learners’ D
ictionary with exercises
�T
he Rosetta S
tone English Library
�C
larity Pronunciation P
ower
�M
astering English in V
ocabulary, Gram
mar, S
pellings, Com
position�
Dorling K
indersley series of Gram
mar, P
unctuation, Com
position etc.�
Language in Use, F
oundation Books P
vt Ltd�
Learning to Speak E
nglish - 4 CD
s�
Microsoft E
ncarta�
Murphy’s E
nglish Gram
mar, C
ambridge
�T
ime series of IQ
Test, B
rain-teasers, Aptitude T
est etc.�
En
glish
in M
ind
, He
rbe
rt Pu
chta
an
d Je
ff Stra
nks w
ith M
ere
dith
Levy,Cam
bridge
Bo
oks S
ug
gested
for E
ng
lish lab
:
1.D
eve
lop
ing
Co
mm
un
icatio
n S
kills by K
rishn
a M
oh
an
& M
ee
ra B
en
erji
(Macm
illan)2.
Speaking E
nglish Effectively by K
rishna Mohan &
NP
Singh (M
acmillan)
3.B
etter English P
ronunciation by JDO
Connor (U
BS
– Cam
bridge)4.
Oxford P
ractice Gram
mar w
ith Answ
ers, John Eastw
ood, Oxford
5.H
andbook of English G
ramm
ar and Usage, M
ark Lester and Larry Beason,
Tata M
cGraw
-Hill
6.A
text book of English P
honetics for Indian Students by T
.Balasubram
anian(M
acmillan)
7.Lingua T
OE
FL C
BT
Insider, by Dream
tech8.
TO
EF
L & G
RE
( KA
PLA
N, A
AR
CO
& B
AR
RO
NS
, US
A, C
racking GR
E by
CLIF
FS
)9.
English S
kills for Technical S
tudents, WB
SC
TE
with B
ritish Council, O
L10.
A H
andbook of English for C
ompetitive E
xaminations, by B
Shyam
ala Rao,
Blakie B
ooks, Chennai.
SC
HE
ME
OF
EV
ALU
AT
ION
—S
ubject: English Language
Laboratory Practice Lab: C
ode—
Practical E
xamination: A
s per University N
orms:
IInternal A
ssessment —
— 25 M
arks
IIE
nd Exam
ination ——
50 Marks
Distrib
utio
n an
d W
eigh
tage o
f Marks
EN
GLIS
H LA
NG
UA
GE
LAB
OR
AT
OR
Y P
RA
CT
ICE
1.T
he practical examinations for the E
nglish Language Laboratory practice shallbe conducted as per the U
niversity norms prescribed for the core engineering
practical sessions.2.
For the E
nglish Language lab sessions, there shall be a continuous evaluationduring the year for 25 sessional m
arks and 50 End E
xamination m
arks. Of the
25 marks, 15 m
arks shall be awarded for day-to-day w
ork and 10 marks to be
awarded by conducting Internal Lab T
est(s). The E
nd Exam
ination shall beconducted by the teacher concerned w
ith the help of another mem
ber of thestaff of the sam
e department of the sam
e institution.
2005-20062005-2006
16
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
II Year B
. Tech
. AE
– I semester
T P
C
4+1 0 4
(MA
05364) MA
TH
EM
AT
ICS
– II
UN
IT – I
Matrices : E
lementary row
transformations – R
ank – Norm
al form - E
chelon form –
Consistency – S
olution of system of sim
ultaneous linear homogeneous and non-
homogeneous equations.
UN
IT – II
Eigen values, eigen vectors – properties – C
ayley-Ham
ilton Theorem
- Inverse andpow
ers of a matrix by C
ayley-Ham
ilton theorem – D
iagonolization of matrix.
Calculation of pow
ers of matrix – M
odal and spectral matrices. R
eal matrices –
Sym
metric, skew
- symm
etric, orthogonal, Linear Transform
ation - Orthogonal
Transform
ation. Com
plex matrices: H
ermitian, S
kew-H
ermitian and U
nitary – Eigen
values and eigen vectors of complex m
atrices and their properties.
UN
IT-III
Quadratic form
s- Reduction of quadratic form
to canonical form – R
ank - Positive,
negative definite - semi definite - index - signature - S
ylvester law.
UN
IT –IV
Fourier S
eries: Determ
ination of Fourier coefficients – F
ourier series – even andodd functions – F
ourier series in an arbitrary interval – even and odd periodiccontinuation – H
alf-range Fourier sine and cosine expansions.
UN
IT-V
Form
ation of partial differential equations by elimination of arbitrary constants and
arbitrary functions – solutions of first order linear (Lagrange) equation and nonlinear(standard type)equations. M
ethod of separation of variables – Classification of second
order linear Partial D
ifferential Equations, solutions of one dim
ensional heat equation,w
ave equation and two-dim
ensional Laplace’s equation under initial and boundaryconditions.
UN
IT –V
IF
ourier integral theorem – F
ourier sine and cosine integrals. Fourier transform
–F
ourier sine and cosine transforms – properties – inverse transform
s – Finite F
ouriertransform
s.
UN
IT-V
IIz-transform
– inverse z-transform - properties – D
amping rule – S
hifting rule – Initialand final value theorem
s. Convolution theorem
– Solution of difference equation by
z-transforms.
UN
IT-V
IIIW
ave lets – The H
aar wavelets – A
wavelet expansion - M
ultiresolution analysisw
ith Haar W
avelets - General construction of w
avelets and multiresolution analysis
- Shannon w
avelets.
TE
XT
BO
OK
S:
1.A
Text book of E
ngineering Mathem
atics Volum
e – II, 2005T
,K.V
.Iyengar, B.K
rishna Gandhi and others, S
.Chand and C
ompany.
2.E
ngineering Mathem
atics, B.V
.Ram
ana, Tata M
cGraw
-Hill 2003.
RE
FE
RE
NC
ES
:1.
En
gin
ee
ring
Ma
the
ma
tics–II, 2
00
2, P
.Na
ge
swa
ra R
ao
, Y.N
arsim
hu
lu,
Prabhakara R
ao
2.E
ngineering Mathem
atics, S.K
.V.S
. Sri R
ama C
hary, M.B
hujanga Rao, S
hankar,
B.S
.Publications 2000.
3.A
dvanced Engineering M
athematics (eighth edition), E
rwin K
reyszig, John Wiley
& S
ons (AS
IA) P
vt. Ltd. 2001.
4.A
dvanced Engineering P
eter V.O
’Neil T
homson B
rooks/Cole.
5.A
dva
nce
d E
ng
ine
erin
g M
ath
em
atics, M
erle
C.P
otte
r, J.L.G
old
be
rg,
E.F
.Abrufadel, O
xford University P
ress. Third E
dition 2005.
6.E
ngineering Mathem
atics – II, 2005, Sankaraiah, V
GS
Book Links, H
yderabad.
2005-20062005-2006
17
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AL
UN
IVE
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ITY
HY
DE
RA
BA
DII Y
ear B. T
ech. A
E – I sem
esterT
P C
4+1 0 4(CS05433) O
BJECT ORIENTED ANALYSIS AND DESIG
N THROUG
H UML
UN
IT-I
INT
RO
DU
CT
ION
TO
UM
L: Importance of m
odeling, principles of modeling, object
orie
nte
d m
od
elin
g, co
nce
ptu
al m
od
el o
f the
UM
L, A
rchite
cture
, So
ftwa
reD
evelopment Life C
ycle.U
NIT
-IIB
AS
IC S
TR
UC
TU
RA
L MO
DE
LING
: Classes, R
elationships, comm
on Mechanism
s,and diagram
s. A
dva
nce
d S
tructu
ral M
od
elin
g: A
dva
nce
d cla
sses, a
dva
nce
d re
latio
nsh
ips,
Interfaces, Types and R
oles, Packages.
UN
IT-III
CLA
SS
& O
BJE
CT
DIA
GR
AM
S: T
erms, concepts, m
odeling techniques for Class
& O
bject Diagram
s.U
NIT
- IVB
AS
IC B
EH
AV
IOR
AL M
OD
ELIN
G-I: Interactions, Interaction diagram
sU
NIT
-VB
AS
IC B
EH
AV
IOR
AL M
OD
ELIN
G-II: U
se cases, Use case D
iagrams, A
ctivityD
iagrams.
UN
IT-V
IA
DV
AN
CE
D B
EH
AV
IOR
AL M
OD
ELIN
G: E
vents and signals, state machines,
processes and Threads, tim
e and space, state chart diagrams.
UN
IT-V
IIA
RC
HIT
EC
TU
RA
L MO
DE
LING
: Com
ponent, Deploym
ent, Com
ponent diagrams
and Deploym
ent diagrams.
UN
IT-V
IIIC
AS
E S
TU
DY
: The U
nified Library applicationT
EX
T B
OO
KS
:1.
Grady B
ooch, James R
umbaugh, Ivar Jacobson : T
he Unified M
odelingLanguage U
ser Guide, P
earson Education.
2.H
ans-Erik E
riksson, Magnus P
enker, Brian Lyons, D
avid Fado: U
ML 2 T
oolkit,W
ILEY
- Dream
tech India Pvt. Ltd.
RE
FE
RE
NC
ES
:1.
Meilir P
age-Jones: Fundam
entals of Object O
riented Design in U
ML, P
earsonE
ducation.2.
Pascal R
oques: Modeling S
oftware S
ystems U
sing UM
L2, WILE
Y-D
reamtech
India Pvt. Ltd.
3.A
tul Kahate: O
bject Oriented A
nalysis & D
esign, The M
cGraw
-Hill C
ompanies.
4.M
ark Priestley: P
ractical Object-O
riented Design w
ith UM
L.5.
Appling U
ML and P
atterns: An introduction to O
bject – Oriented A
nalysis andD
esign and Unified P
rocess, Craig Larm
an, Pearson E
ducation.
JAW
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TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DII Y
ear B. T
ech. A
E – I sem
esterT
P C
4+1 0 4
(CE
05375) ME
CH
AN
ICS
OF
SO
LID
S
UN
IT – I
SIM
PLE
ST
RE
SS
ES
AN
D S
TR
AIN
SE
lasticity and plasticity – Types of stresses and strains – H
ooke’s law – stress –
strain diagram for m
ild steel – Working stress – F
actor of safety – Lateral strain,P
oisson’s ratio and volumetric strain – E
lastic moduli and the relationship betw
eenthem
– Bars of varying section – com
posite bars – Tem
perature stresses.S
train energy – Resilience – G
radual, sudden, impact and shock loadings.
UN
IT – II
SH
EA
R F
OR
CE
AN
D B
EN
DIN
G M
OM
EN
T
Definition of beam
– Types of beam
s – Concept of shear force and bending m
oment
– S.F
and B.M
diagrams for cantilver, sim
ply supported and overhanging beams
subjected to point loads, u.d.l., uniformly varying loads and com
bination of theseloads – P
oint of contraflexure – Relation betw
een S.F
., B.M
and rate of loading at asection of a beam
.
UN
IT – III
FLE
XU
RA
L ST
RE
SS
ES
Th
eo
ry of sim
ple
be
nd
ing
– A
ssum
ptio
ns –
De
rivatio
n o
f be
nd
ing
eq
ua
tion
:M
/I = f/y =
E/R
Neutral axis – D
etermination bending stresses – section m
odulus ofrectangular and circular sections (S
olid and Hollow
), I,T,A
ngle and Channel sections
– Design of sim
ple beam sections.
UN
IT – IV
SH
EA
R S
TR
ES
SE
SD
erivation of formula – S
hear stress distribution across various beams sections like
rec tangular, circular, triangular, I, T angle sections.
UN
IT – V
AN
ALY
SIS
OF
PIN
-JOIN
TE
D P
LAN
E F
RA
ME
S :
Determ
ination of Forces in m
embers of plane, pin-joined, perfect trusses by (i) m
ethodof joints and (ii) m
ethod of sections. Analysis of various types of cantilever and
simply – supported trusses.- by m
ethod of joints, method of sections and tension
coefficient methods.
2005-20062005-2006
18
UN
IT – V
ID
EF
LEC
TIO
N O
F B
EA
MS
Bending into a circular arc – slope, deflection and radius of curvature – D
ifferentialequation for the elastic line of a beam
– Double integration and M
acaulay’s methods
– Determ
ination of slope and deflection for cantilever and simply supported beam
ssubjected to point loads, - U
.D.L uniform
ly varying load. Mohr’s theorem
s – Mom
entarea m
ethod – application to simple cases including overhanging beam
s.
UN
IT – V
IIT
HIN
CY
LIND
ER
S
Th
in se
am
less cylin
drica
l she
lls – D
eriva
tion
of fo
rmu
la fo
r lon
gitu
din
al a
nd
circumferential stresses – hoop, longitudinal and V
olumetric strains – changes in
dia, and volume of thin cylinders – R
iveted boiler shells – Thin spherical shells.
UN
IT – V
IIIT
hick cylinders – lame’s equation – cylinders subjected to inside and out side
pressures – compound cylinders.
TE
XT
BO
OK
S :
1.S
trength of Materials by A
ndrew P
ytel and Ferdinond L. S
inger Longman.
2.S
trength of Materials by Jondar; G
algotia Publications.
RE
FE
RE
NC
ES
:1.
Strength of M
aterials by Bensal, Lakshm
i Publications.
2.S
trength of Materials by S
.Tum
oshenko.3.
Strength of M
aterials by R.S
.Khurm
i; S.C
hand & C
o. 2005.
JAW
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TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DII Y
ear B. T
ech. A
E – I sem
esterT
P C
4+1 0 4(C
E05374) M
EC
HA
NIC
S O
F F
LU
IDS
UN
IT – IFluid Properties A
nd Fluid Statics: Density, Specific w
eight, Specific gravity, viscosity, Vapourpressure, com
pressibility, Pressure at a point, Pascal’s law, pressure variation with tem
perature,density and attitude. H
ydro static law, Piezometer, Sim
ple and differential manom
eters, pressuregauges, total pressure and center of pressure – plane, vertical and inclined surfaces. Buoyancyand stability of floating bodies.U
NIT – II
Fluid Kinem
atics : Stream line, path line, streak line, stream
tube, classification of flows, steady,
unsteady, uniform, non-uniform
, laminar, turbulent, rotational, irrotational flow
s, one, two and three
dimensional flow
s – Continuity equation in 3D
flow, stream function, velocity potential function.
UN
IT – IIIFluid D
ynamics : Surface and Body forces – Euler’s and Bernoulli’s equation derivation, N
avier-stokes equation (explanation only) M
omentum
equation - applications, vortex – Free and Forced.Forced vortex w
ith free surface.U
NIT – IV
Similitude and Flow
Measurem
ent – Similarly law
s, distorted models. Flow
through Venturimeters
and Orificem
eter, flow through notches and w
eirs, Viscometers, H
ot wire Anem
ometers, Pitot tube,
Flow through nozzles.
UN
IT – VA
pproximate solutions of N
.S. E
quations - Boundary layer- concepts, P
randtlcontribution,C
haracteristices of boundary layer along a thin flat plate Von-karman’s m
omentum
integral equation (No derivation), lam
inar and turbulent Boundary layers,BL in transition,separationof BL,control of BL separation,flow
around submerged objects, D
rag and lift – types of drag –m
agnus effect.U
NIT – VI
Closed C
onduit Flow: C
haracteristics of real fluids – Reynolds experim
ent –Darcy’s equation,
Minor losses – pipes in series – pipes in parallel – Total energy line and hydraulic gradient line.
UN
IT VIIExact Solutions of N
avier Stokes Equations. Flow betw
een parallel plates, flow through long
tubes - Fow through inclined tubes, Turbulent flow, variation of friction factor w
ith Reynold’s N
umber
– Mody’s chart.
UN
IT VIIIFlow
of Com
pressible Fluid: Introduction, Thermodynam
ic relations, basic equations ofcom
pressible flow, velocity of sound wave in a fluid for isotherm
al and adiabatic process, mach
number and its applications, m
ach angle, Propagation of Pressure waves and stagnation properties
TEXT BO
OK
S:1.
Fluid Mechanics H
ydraulics and Hydraulics M
achines Modi & Seth, Standard publications,
New
Delhi.
2.Engineering Fluid M
echanics by K.L.Kumar, S.C
hand & Co.
REFER
ENC
ES :1.
Fluid Mechanics – Frank in w
hite Mc-G
rawhill.
2.Fluid M
echanics - John – F.Dauglas, Pearson Educations publishers.
3.Fluid M
echanics & Hydraulic M
achines - D. R
amadurgaiah, N
ewage Publishers.
2005-20062005-2006
19
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AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DII Y
ear B. T
ech. A
E – I sem
esterT
P C
0 – 6 – 4(A
E05026) A
IRC
RA
FT
EN
GIN
EE
RIN
G D
RA
WIN
GU
NIT
:IM
achine Draw
ing conventions. Need for D
rawings conventions – Introduction to
ISI- C
onventionsa)
Conventional representation of m
aterials , comm
on machine elem
entsand parts such as screw
s,nuts,bolts,keys,gears,webs,ribs
b)T
ypes of sections – Selection of sectional planes and draw
ing of sectionsand auxiliary sectional view
s. Parts not usually sectioned
c)M
ethods of dimensioning , general rules for sizes and placem
ent ofdim
ensions for holes ,centers, curved and Tapered features
d)T
itle boxes, their size, location and details –comm
on abbreviations andtheir liberal usage.
e)T
ypes of drawing – w
orking drawing for m
achine partsU
NIT
: IID
rawing of M
achine Elem
ents and simple parts .S
ection of views , additional view
sfor the follow
ing machine elem
ents and parts with every draw
ing proportionsa)
Popular form
s of screw threads, bolts, set screw
s and bolted joints.b)
Keys,cottered joint and knuckle joint
c)R
iveted joints for plates.d)
Shaft couplings, spigot and socket pipe joint.
e)Journal, pivot, collar and foot step bearing
f)W
elded joints and welding sym
bols.U
NIT
: IIIF
ollowing sim
ple Air C
raft assembly draw
ings only.a)
Diffe
ren
t type
s of tru
sses u
sed
in w
ing
s fuse
lag
e in
clud
ing
ribs,
striengers,skin,braketsb)
Different elem
ents of fuselage structures ,bulk head , rings ( frame) long irons
c)D
ifferent types of fuselage.d)
landing gear basic elements ,structural brackets ,w
heel, shock absorber andH
ydraulic cylindere)
connecting rod for aero piston engineT
ext Bo
oks:
1.M
achine drawing by N
.D. B
aht / V.M
. Panchal / C
harotar Publication H
ouse –2000 E
d .2.
Air C
raft structures BY
TM
H M
egsonR
EF
ER
EN
CE
S:
1.M
achine Draw
ing by K.L.N
arayana, P.K
annaiah and K.V
enkata Reddy / N
ewA
ge Publishers.
2.A
ir Craft structures by B
ruhn.E.H
3.M
achine Draw
ing by P.S
.Gill
4.M
achine Draw
ing by Luzzader5.
Machine D
rawing by R
ajput.
JAW
AH
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TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DII Y
ear B. T
ech. A
E – I sem
esterT
P C
4+1 0 4(C
E 05239) E
NV
IRO
NM
EN
TA
L S
TU
DIE
SU
NIT
- I
Mu
ltidiscip
linary n
ature o
f En
viron
men
tal Stu
dies: D
efinition, Scope and
Importance – N
eed for Public A
wareness.
UN
IT - II
Natu
ral Reso
urces : R
enewable and non-renew
able resources – Natural resources
and associated problems – F
orest resources – Use and over – exploitation,
deforestation, case studies – Tim
ber extraction – Mining, dam
s and other effects onforest and tribal people – W
ater resources – Use and over utilization of surface and
ground water – F
loods, drought, conflicts over water, dam
s – benefits and problems
- Mineral resources: U
se and exploitation, environmental effects of extracting and
using mineral resources, case studies. - F
ood resources: World food problem
s,changes caused by agriculture and overgrazing, effects of m
odern agriculture,fertilizer-pesticide problem
s, water logging, salinity, case studies. - E
nergy resources:G
rowing energy needs, renew
able and non-renewable energy sources use of
alternate energy sources. Case studies. Land resources: Land as a resource, land
degradation, man induced landslides, soil erosion and desertification. R
ole of anindividual in conservation of natural resources. E
quitable use of resources forsustainable lifestyles.
UN
IT - III
Eco
systems : C
oncept of an ecosystem. - S
tructure and function of an ecosystem.
- Producers, consum
ers and decomposers. - E
nergy flow in the ecosystem
-E
cological succession. - Food chains, food w
ebs and ecological pyramids. -
Introduction, types, characteristic features, structure and function of the following
ecosystem:
a. Forest ecosystem
b. Grassland ecosystem
c. Desert ecosystem
d. Aquatic ecosystem
s (ponds, streams, lakes, rivers, oceans, estuaries)
UN
IT - IV
Bio
diversity an
d its co
nservatio
n : Introduction - D
efinition: genetic, species andecosystem
diversity. - Bio-geographical classification of India - V
alue of biodiversity:consum
ptive use, productive use, social, ethical, aesthetic and option values - .B
iodiversity at global, National and local levels. - . India as a m
ega-diversity nation- H
ot-sports of biodiversity - Threats to biodiversity: habitat loss, poaching of w
ildlife,m
an-wildlife conflicts. - E
ndangered and endemic species of India - C
onservation ofbiodiversity: In-situ and E
x-situ conservation of biodiversity.
2005-20062005-2006
20
UN
IT - V
En
viron
men
tal Po
llutio
n : D
efinition, Cause, effects and control m
easures of :
a.A
ir pollution
b.W
ater pollution
c.S
oil pollution
d.M
arine pollution
e.N
oise pollution
f.T
hermal pollution
g.N
uclear hazards
So
lid w
aste Man
agem
ent : C
auses, effects and control measures of urban and
industrial wastes. - R
ole of an individual in prevention of pollution. - Pollution case
studies. - Disaster m
anagement: floods, earthquake, cyclone and landslides.
UN
IT - V
I
So
cial Issues an
d th
e En
viron
men
t : Fro
m U
nsu
stain
ab
le to
Su
stain
ab
ledevelopm
ent -Urban problem
s related to energy -Water conservation, rain w
aterharvesting, w
atershed managem
ent -Resettlem
ent and rehabilitation of people; itsproblem
s and concerns. Case S
tudies -Environm
ental ethics: Issues and possiblesolutions. -C
limate change, global w
arming, acid rain, ozone layer depletion, nuclear
accidents and holocaust. Case S
tudies. -Wasteland reclam
ation. -Consum
erismand w
aste products. -Environm
ent Protection A
ct. -Air (P
revention and Control of
Pollution) A
ct. -Water (P
revention and control of Pollution) A
ct -Wildlife P
rotectionA
ct -Forest C
onservation Act -Issues involved in enforcem
ent of environmental
legislation. -Public aw
areness.
UN
IT - V
II
Hu
man
Po
pu
lation
and
the E
nviro
nm
ent : P
opulation growth, variation am
ongnations. P
opulation explosion - Fam
ily Welfare P
rogramm
e. -Environm
ent and human
health. -Hum
an Rights. -V
alue Education. -H
IV/A
IDS
. -Wom
en and Child W
elfare. -R
ole of information T
echnology in Environm
ent and human health. -C
ase Studies.
UN
IT - V
III
Field
wo
rk : Visit to a local area to docum
ent environmental assets R
iver /forestg
rassla
nd
/hill/m
ou
nta
in -V
isit to a
loca
l po
llute
d site
-Urb
an
/Ru
ral/in
du
strial/
Agricultural S
tudy of comm
on plants, insects, birds. -Study of sim
ple ecosystems-
pond, river, hill slopes, etc.
TE
XT
BO
OK
:
Textbook of E
nvironmental S
tudies for Undergraduate C
ourses by Erach B
haruchafor U
niversity Grants C
omm
ission.
JAW
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TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
II Year B
. Tech
. AE
– I semester
T P
C
0 – 3 – 2
(CS
05564) UM
L L
AB
1.T
he student should take up the case study of Unified Library application w
hich
is mentioned in the theory, and M
odel it in different views i.e U
se case view,
logical view, com
ponent view, D
eployment view
, Database design, forw
ard
and Reverse E
ngineering, and Generation of docum
entation of the project.
2.S
tudent has to take up another case study of his/her own interest and do the
same w
hat ever mentioned in first problem
. Som
e of the ideas regarding case
studies are given in reference books which w
ere mentioned in theory syllabus
can be referred for some idea.
2005-20062005-2006
21
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CH
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LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DII Y
ear B. T
ech. A
E – I sem
esterT
P C
0 – 3 – 2
(CE05377) M
ECH
NIC
S OF SO
LIDS &
MEC
HA
NIC
S OF FLU
IDS LA
B
ME
CH
AN
ICS
OF
SO
LID
S L
AB
1.D
irect tension test
2.B
ending test ona)
Sim
ple supportedb)
Cantilever beam
3.T
orsion test
4.H
ardness testa)
Brinells hardness test
b)R
ockwell hardness test
5.T
est on springs
6.C
ompression test on cube
7.Im
pact test
8.P
unch shear test
ME
CH
AN
ICS
OF
FL
UID
S L
AB
1.C
alibration of Venturim
eter2.
Calibration of O
rifice meter
3.D
etermination of C
oefficient of discharge for a small orifice by a constant head
method.
4.D
etermination of C
oefficient of discharge for an external mouth piece by variable
head method.
5.C
alibration of contracted Rectangular N
otch6.
Calibration of contracted T
riangular Notch
7.D
etermination of C
oefficient of loss of head in a sudden contraction and frictionfactor.
8.V
erification of Bernoulli’s equation.
JAW
AH
AR
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L N
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TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DII Y
ear B. T
ech. A
E – II sem
esterT
P C
4+1 0 4(M
A05366) M
ATHEM
ATICS FO
R A
ERO
SPAC
E ENG
INEER
SUNIT -ISPECIAL FUNCTIO
NS: Gam
ma and beta functions and their properties. Evaluation of im
proper integrals.Bessel functions – Properties – R
ecurrence relations. Orthogonality of Bessel functions. Legendre
functions –Legendra Polynomials- properties-recurrence relations. O
rthogonality of Legendre polynomials-
Rodrigue’s formula
UNIT- IIFunctions of a com
plex variable –continuity-differentiability –analyticity- properties of analytic functions.Cauchy – Riem
ann equations in Cartesian and polar co- ordinates .Harmonic and conjugate harm
onicfunctions. M
ilne – Thomson m
ethod, complex integration.
UNIT- IIILine integral – evaluation along a path and by indefinite integration – Cauchy integral theorem
- Cauchyintegral form
ula. Generalized integral form
ula- zero- singular point- isolated singular point – pole oforder, m
– essential singularityUNIT- IVCom
plex power series: radius of convergence – Expansion in Taylor’s series , Maclaurins series and
Laurent’s series.Residue: Evaluation of residue by form
ula and by Laurent series – Residue theorem –Evaluation of
Integrals of type ? f(cosθ, sinθ) dθ, ?f(x) dx ,?eim
x f(x) dx; Argument principle- Rouche’s theorem
–fundam
ental theorem of algebra. Liou ville’s theorem
UNIT- V:Conform
al mapping, Transform
ation by ez , log e z z n , sinz ,cosz , z+ n/z . Bilinear transform
ation – fixedpoint, cross ratio, properties, invariance of cross ratio under bilinear transform
ation. Determination of
bilinear transformation m
apping 3 given points.UNIT- VITensor analysis: Introduction to tensor analysis. Sum
mation to convention- co –variant and contravariant
tensors- Fundamental and reciprocal tensors and christoffel sym
bols.UNIT-VIISTATISTICS: Sam
ple space and events – probability, the axioms of probability –som
e elementary
theorems- conditional probability- Baye’s theorem
UNIT - VIIIIntroduction to random
variables – discrete and continuous- discontinuous functions. Binomial, Poisson
and normal distributions and related properties, m
ean, standard deviation, auto and cross correlations.TEXT BO
OKS:
1.A text book of engineering m
athematics vol iv-2004 by T.K.Iyengar, B.Krishna G
andhi & Others,
S.Chand and company.
2.Engineering M
athematics – B.V.Ram
ana BY Tata Mc-G
rawhill.REFERENCES:1.
Fundamentals of M
athematical statistics by S.C. G
upta and VK Kapoor.2.
Brog .S.F. Matrix – Tensor m
ethods in Continuum M
echanics- D- VAN Nostrand company.
2005-20062005-2006
22
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TE
CH
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LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DII Y
ear B. T
ech. A
E – II sem
esterT
P C
4+1 0 4(A
E05016) A
ER
OD
YN
AM
ICS
– IU
NIT
-I - BA
SIC
SW
ing and Airfoil section geom
etry - Aerodynam
ic forces and mom
ents-Force and
mom
ent components and coefficients, P
ressure distribution on an airfoil, Types of
drag, Estim
ation of lift, Drag and pitching m
oment coefficient from
the pressuredistribution. E
xperimental m
ethods, wake survey.
UN
IT-II - E
LE
ME
NT
AR
Y F
LO
WS
Incompressible flow
condition, Governing equation for irrotational, incom
pressibleflow
: Laplace’s equation, Boundary conditions. E
lementary flow
s. Com
bination ofuniform
flow w
ith a Source and S
ink, Doublet. F
low over a circular cylinder, V
ortexflow
. Circulation, K
utta-Joukowski theorem
. Lifting flow over a cylinder T
he vortexsheet. K
elvin circulation theorem and starting vortex.
UN
IT-III - IN
CO
MP
RE
SS
IBL
E F
LO
W O
VE
R A
IRF
OIL
ST
he complex potential function and conform
al transformation, T
he Kutta-Z
hukovskytransform
ation. Kutta condition. Lift on the Z
hukovsky airfoil section.U
NIT
-IV - T
HIN
AIR
FO
IL T
HE
OR
YC
lassical thin airfoil theory for symm
etric and cambered airfoil sections. C
omparison
of theoretical and experimental results. Lim
itations of thin airfoil theory.U
NIT
-V - IN
CO
MP
RE
SS
IBL
E F
LO
W O
VE
R F
INIT
E W
ING
SV
ortex filament, B
iot-Savart law
and Helm
holtz’s theorems, P
randtls classical liftingline theory: D
ownw
ash and induced drag. Elliptical and m
odified elliptical liftdistribution. Lift distribution on w
ings. Limitations of P
randtl’s lifting line theory.U
NIT
-VI - E
XT
EN
DE
D L
IFT
ING
LIN
E T
HE
OR
YE
xtended lifting line theory- lifting surface theory, vortex lattice method for w
ings.Lift, drag and m
oment characteristics of com
plete airplane.U
NIT
-VII - S
OU
RC
E P
AN
EL
ME
TH
OD
Source panel m
ethod-non-lifting flow over an arbitrary bodies-potential flow
over acircular cylinder.U
NIT
-VIII - V
OR
TE
X P
AN
EL
ME
TH
OD
Vortex panel m
ethods-Lifting flow over an arbitrary body- flow
over a symm
etricalairfoilT
EX
T B
OO
KS
1.A
nderson, J .D., F
undamental of A
erodynamics, M
c Graw
-Hill International
Edition
2.H
oughton, E.L., and C
arruthers, N.B
., Aerodynam
ics for Engineering S
tudents,E
dward A
rnold Publishers Ltd., London, 1989
RE
FE
RE
NC
ES
:1.
Clancy, L.J., A
erodynamics, P
itman, 1986
2.M
ilne Thom
son, Theoretical A
erodynamics, M
acmillan, 1985
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DII Y
ear B. T
ech. A
E – II sem
esterT
P C
4+1 0 4(M
E05551) T
HE
RM
OD
YN
AM
ICS
Tab
les/Co
des: S
team T
ables an
d M
ollier C
hart, R
efrigeratio
n T
ables
sho
uld
be su
pp
lied
UN
IT – I
System
, Control V
olume, S
urrounding, Boundaries, U
niverse, Types of S
ystems,
Macroscopic and M
icroscopic viewpoints, C
oncept of Continuum
, Therm
odynamic
Equilibrium
, State, P
roperty, Process, C
ycle – Reversibility – Q
uasi – static Process,
Irreversible Process, C
auses of Irreversibility – Energy in S
tate and in Transition,
Types, W
ork and Heat, P
oint and Path function.
UN
IT II
Zeroth Law
of Therm
odynamics – C
oncept of quality of Tem
perature – Principles of
Therm
ometry – R
eference Points – C
onst. Volum
e gas Therm
ometer – S
cales ofT
emperature, Ideal G
as Scale – P
MM
I - Joule’s Experim
ents – First law
ofT
hermodynam
ics – Corollaries – F
irst law applied to a P
rocess – applied to a flowsystem
– Steady F
low E
nergy Equation.
UN
IT – III
Limitations of the F
irst Law – T
hermal R
eservoir, Heat E
ngine, Heat pum
p ,P
arameters of perform
ance, Second Law
of Therm
odynamics, K
elvin-Planck and
Clausius S
tatements and their E
quivalence / Corollaries, P
MM
of Second kind,
Carnot’s principle, C
arnot cycle and its specialties, Therm
odynamic scale of
Tem
perature, Clausius Inequality, E
ntropy, Principle of E
ntropy Increase – Energy
Equation, A
vailability and Irreversibility – Therm
odynamic P
otentials, Gibbs and
Helm
holtz Functions, M
axwell R
elations – Elem
entary Treatm
ent of the Third Law
of Therm
odynamics.
UN
IT IV
Pure S
ubstances, p-V-T
- surfaces, T-S
and h-s diagrams, M
ollier Charts, P
haseT
ransformations – T
riple point at critical state properties during change of phase,D
ryness Fraction – C
lausius – Clapeyron E
quation Property tables. M
ollier charts –V
arious Therm
odynamic processes and energy T
ransfer – Steam
Calorim
etry.
2005-20062005-2006
23
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DII Y
ear B. T
ech. A
E – II sem
esterT
P C
4+1 0 4(EE05187) ELEC
TRIC
AL A
ND
ELECTR
ON
ICS EN
GIN
EERIN
GU
NIT
-I - EL
EC
TR
ICA
L C
IRC
UIT
SB
asic definitions, Types of elem
ents, Ohm
’s Law, R
esistive networks, K
irchhoff’sLaw
s, Inductive networks, capacitive netw
orks, Series, P
arallel circuits and Star-
delta and delta-star transformations.
UN
IT II - D
C M
AC
HIN
ES
Principle of operation of D
C G
enerator – emf equation - types – D
C m
otor types –torque equation – applications – threee point starter.U
NIT
III - TR
AN
SF
OR
ME
RS
Principle of operation of single phase transform
ers – emf equation – losses – efficiency
and regulationU
NIT
IV - A
C M
AC
HIN
ES
Principle of operation of alternators – regulation by synchronous im
pedance method
– Principle of operation of induction m
otor – slip – torque characteristics – applications.U
NIT
V - IN
ST
RU
ME
NT
SB
asic Principle of indicating instrum
ents – permanent m
agnet moving coil and m
ovingiron instrum
ents.U
NIT
VI
- DIO
DE
AN
D IT
’S C
HA
RA
CT
ER
IST
ICS
P-n junction diode, sym
bol, V-I C
hacracteristics, Diode A
pplications, Rectifiers –
Half w
ave, Full w
ave and Bridge rectifiers (sim
ple Problem
s)U
NIT
VII- T
RA
NS
IST
OR
SP
NP
and NP
N Junction transistor, T
ransistor as an amplifier, S
CR
characteristicsand applicationsU
NIT
VIII - C
AT
HO
DE
RA
Y O
SC
ILL
OS
CO
PE
Principles of C
RT
(Cathode R
ay Tube), D
eflection, Sensitivity, E
lectrostatic andM
ag
ne
tic de
flectio
n, A
pp
licatio
ns o
f CR
O - V
olta
ge
, Cu
rren
t an
d fre
qu
en
cym
easurements.
TE
XT
BO
OK
S:
1.E
ssentials of Electrical and C
omputer E
ngineering by David V
. Kerns, JR
. J.D
avid Irwin
2.P
rinciples of Electrical and E
lectronics Engineering by V
.K.M
ehta, S.C
hand &C
o.R
EF
ER
EN
CE
S:
1.Introduction to E
lectrical Engineering – M
.S N
aidu and S. K
amakshaiah, T
MH
Publ.
2.B
asic Electrical E
ngineering by Kothari and N
agarath, TM
H P
ublications, 2nd
Edition.
UN
IT - V
Perfect G
as Laws – E
quation of State, specific and U
niversal Gas constants – various
Non-flow
processes, properties, end states, Heat and W
ork Transfer, changes in
Internal Energy – T
hrottling and Free E
xpansion Processes – F
low processes –
De
viatio
ns fro
m p
erfe
ct Ga
s Mo
de
l – V
an
de
r Wa
als E
qu
atio
n o
f Sta
te –
Com
pressibility charts – variable specific Heats – G
as Tables
UN
IT – V
I
Mixtures of perfect G
ases – Mole F
raction, Mass friction G
ravimetric and volum
etricA
nalysis – Dalton’s Law
of partial pressure, Avogadro’s Law
s of additive volumes –
Mole fraction , V
olume fraction and partial pressure, E
quivalent Gas const. A
ndM
olecular Internal Energy, E
nthalpy, sp. Heats and E
ntropy of Mixture of perfect
Ga
ses a
nd
Va
po
ur, A
tmo
sph
eric a
ir - Psych
rom
etric P
rop
ertie
s – D
ry bu
lbT
emperature, W
et Bulb T
emperature, D
ew point T
emperature, T
hermodynam
ic Wet
Bulb T
emperature, S
pecific Hum
idity, Relative H
umidity, saturated A
ir, Vapour
pressure, Degree of saturation – A
diabatic Saturation , C
arrier’s Equation –
Psychrom
etric chart.
UN
IT - V
IIP
OW
ER
CY
CL
ES
Otto, D
iesel, Dual C
ombustion cycles, S
terling Cycle, A
tkinson Cycle, E
riccson Cycle,
Lenoir Cycle – D
escription and representation on P–V
and T-S
diagram, T
hermal
Efficiency, M
ean Effective P
ressures on Air standard basis – com
parison of Cycles.
UN
IT V
IIIR
EF
RIG
ER
AT
ION
CY
CL
ES
Brayton and R
ankine cycles – Perform
ance Evaluation – com
bined cycles, Bell-
Colem
an cycle, Vapour com
pression cycle-performance E
valuation.
TE
XT
BO
OK
S :
Engineering T
hermodynam
ics / PK
Nag /T
MH
, III Edition
RE
FE
RE
NC
ES
:
1.F
undamentals of C
lassical Therm
odynamics – G
. Van W
ylan & R
.E. S
onntag– John W
iley Pub.
2.E
ngineering Therm
odynamics – Jones &
Dugan
3.T
hermodynam
ics – An E
ngineering Approach – Y
unus Cengel &
Boles /T
MH
4.T
hermodynam
ics – J.P.H
olman / M
cGraw
Hill
5.A
n introduction to Therm
odynamics / Y
VC
Rao / N
ew A
ge
2005-20062005-2006
24
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DII Y
ear B. T
ech. A
E – II sem
esterT
P C
4+1 0 4(AE05333) INTRO
DUCTION TO
AEROSAPCE TRANSPO
RTATION SYSTEM
S
UN
IT-I - T
RA
NS
PO
RT
AT
ION
SY
ST
EM
S
Transportation as a hum
an activity - significance - principal modes – applications.
History of the developm
ent of transportation systems including aviation and space
flight - some landm
arks.
UN
IT-II - A
VIA
TIO
N
The A
tmospheric F
light – Science and T
echnology
The atm
osphere – properties. Principles of atm
ospheric flight – aerostatic andaerodynam
ic forces. Generation of lift and thrust and reduction of drag - aerodynam
icefficiency - the stream
lined body.
UN
IT-III - T
HE
FL
IGH
T V
EH
ICL
E
Flight vehicle configurations- T
he Airplane-construction, D
escription of principalcom
ponents - functions.
UN
IT-IV
- PE
RF
OR
MA
NC
E O
F F
LIG
HT
VE
HIC
LE
S
Perform
ance, stability and control of flight vehicles- relation to design features andconstruction. S
tructural loads on Airfram
e – requirements - principal structural design
features.
UN
IT-V
- AIR
TR
AN
SP
OR
T O
PE
RA
TIO
NS
Purpose, role and m
ission of Civil and M
ilitary flight vehicles. Flight planning,
navigation, air traffic managem
ent, maintenance, ground support, airport and
passenger facilitation systems – principal features.
UN
IT-V
I - AIR
SA
FE
TY
AN
D S
EC
UR
ITY
Air safety- airw
orthiness of aircraft equipment - safety of operations. C
ivil and Military
Aviation regulatory agencies- role in prescribing and m
aintaining air safety standards.
UN
IT-V
II - SP
AC
E T
RA
NS
PO
RT
AT
ION
The high altitude and space environm
ent. Space vehicles- rockets, m
issiles, earthsatellites, space probes, and space stations- applications.
UN
IT-V
III - AV
ION
ICS
The role of avionics in the navigation, guidance and control of flight vehicles.
TE
XT
BO
OK
S
1.A
nderson J.D. , “Introduction to flight” , M
cGraw
Hill, 1995.
2.K
ermode, A
.C. , “F
light without F
ormulae”, M
cGraw
Hill, 1987
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DII Y
ear B. T
ech. A
E – II sem
esterT
P C
4+1 0 4(A
E05378) M
EC
HA
NIS
MS
AN
D M
EC
HA
NIC
AL
DE
SIG
N
UN
IT - I
ME
CH
AN
ISM
S
Elem
ents of links – Classification – R
igid link, flexible and fluid link – Types of
kinematic pairs – S
liding, turning, rolling, screw and spherical pairs – Low
er adhigher pairs – C
losed and open pairs – Constrained m
otion – Com
pletely, partiallyor successfully constrained and incom
pletely constrained.
MA
CH
INE
SM
echanism and m
achines – Classification of m
achines – Kinem
atic chain – Inversionof m
echanism – Inversion of quadratic cycle, C
hain – single and double slider crankchains.
UN
IT – II
ST
RA
IGH
T L
INE
MO
TIO
N M
EC
HA
NIS
MS
Exact and approxim
ate copiers and generated types – Peaucellier, H
art and Scott
Russul – G
rasshopper – Watt T
. Chebicheff and R
obert Mechanism
s and straightline m
otion, Pantograph.
UN
IT – III
KIN
EM
AT
ICS
Velocity and acceleration – M
otion of link in machine – D
etermination of velocity
and acceleration diagrams – G
raphical method – A
pplication of relative velocitym
ethod four bar chain.
AN
AL
YS
IS O
F M
EC
HA
NIS
MS
Analysis of slider crank chain for displacem
ent, Velocity and acceleration of sliding
– Acceleration diagram
for a given mechanism
, Kleins construction, C
oriolisacceleration, D
etermination of C
oriolis component of acceleration.
UN
IT – IV
PL
AN
E M
OT
ION
OF
BO
DY
Instantaneous center of rotation, centroids and axodes – Relative m
otion between
two bodies – T
hree centers in line theorem – G
raphical determination of instantaneous
center, diagrams for sim
ple mechanism
s and determination of angular velocity of
points and links.
2005-20062005-2006
25
UN
IT – V
CA
MS
Definition of cam
and followers – T
heir uses – Types of follow
ers and cams –
Term
inology – Types of follow
er motion – U
niform velocity – S
imple harm
onic motion
and uniform acceleration. M
aximum
velocity and Maxim
um acceleration during out
ward and return strokes in all the above three cases.
UN
IT – V
IA
NA
LY
SIS
OF
MO
TIO
N O
F F
OL
LO
WE
RS
Roller follow
er – Circular cam
with straight, concave and convex flanks.
UN
IT – V
IID
ES
IGN
OF
MA
CH
INE
EL
EM
EN
TS
Principles of m
echanical design- dimensional tolerances, fits.
Design of com
mon m
achine elements
Springs, shafts, couplings, U
niversal coupling.
UN
IT – V
IIIG
EA
RS
AN
D G
EA
R T
RA
INS
Intro
du
ction
to g
ea
rs-type
s, La
w o
f ge
arin
g, T
oo
th p
rofile
s, spe
cificatio
ns,
classification-Helical, B
evel and worm
gears:S
imple and reverted gear train, epicyclic gear trains-velocity ratio or train value
TE
XT
BO
OK
S1.
Theory of M
achines, Dr Jagdish Lal, JM
Shaw
.2.
Theory of M
achines, PL B
allaney, Khanna P
ublishers, 2003.
RE
FE
RE
NC
ES
1.T
heory of Mechanism
s and machines, A
mithab G
hosh and Asok K
umar M
alik,E
ast West P
ress Private Lim
ited – 2001.2.
Theory of M
achines, Abdulla S
harif, Dhanpat R
ai, 1987.3.
Mechanism
and Machine T
heory, JS R
ao and RV
Dukkipati / N
ew A
ge – 1996.4.
Theory of M
achines Through S
olved Problem
s, JS R
ao / New
Age – 1996.
5.M
achine Design P
andya & S
ha - Charotar P
ublication House – 1997.
6.M
echanical Engineering and D
esign, J.E.S
higley and Charles.R
.Mischke,
TM
H, 2003.
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
II Year B
. Tech
. AE
– II semester
T P
C
0 – 3 – 2
(AE
05107) CA
D L
AB
1.F
undamentals of C
AD
and Design process
2.G
eometric M
odeling
-2D
Draw
ings: points, lines, curves, and planes
-3D
Draw
ings: Solids (B
oolean operations)
-P
art Draw
ings and Dim
ensioning
-P
art modeling through 2D
, 3D m
odeling techniques.
3.S
olid and Surface M
odeling
-2D
Draw
ing:
-3D
Draw
ing:
-P
art Draw
ing and Dim
ensioning from A
ircraft Draw
ing
-P
art modeling from
Aircraft C
omponents
-S
olid and surface modeling.
TE
XT
BO
OK
S
1.M
ikell, P., G
roover, “Autom
ation System
s and CIM
”; Prentice H
all of India
2.Ibrahim
Zeid, “C
AD
/CA
M T
heory and Practice”; P
rentice Hall of India
RE
FE
RE
NC
ES
1.S
tephen J. Kochen &
Patrick II. W
ood. “Exploring the U
NIX
System
”;
Techm
edia, 1999.
2.C
AD
/CA
M B
y P.N
.Rao.
2005-20062005-2006
26
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
II Year B
. Tech
. AE
– II semester
T P
C0 – 3 – 2
(EE
05188) EL
EC
TR
ICA
L &
EL
EC
TR
ON
ICS
LA
B
Sectio
n A
: Electrical E
ng
ineerin
g
The follow
ing experiments are required to be conducted as com
pulsoryexperim
ents :
1.S
winburne’s test on D
.C. S
hunt machine. (P
redetermination of efficiency of a
given D.C
. Shunt m
achine working as m
otor and generator).
2.O
C and S
C tests on single phase transform
er (Predeterm
ination of efficiecyand regulation at given pow
er factors)
3.B
rake
test o
n 3
-ph
ase
Ind
uctio
n m
oto
r (De
term
ina
tion
of p
erfo
rma
nce
characteristics)
4.R
egulation of alternator by Synchronous im
pedance method.
In addition to the above four experiments, any one of the experim
ents from the
following list is required to be conducted :
5.S
peed control of D.C
. Shunt m
otor by
a.A
rmature V
oltage control motor
b.F
ield flux control method
6.B
rake test on D.C
Shunt M
otor
Sectio
n B
: Electro
nics E
ng
ineerin
g
1.T
ransistor CE
Characteristics (Input and O
utput)
2.F
ull wave R
ectifier with and w
ithout filters.3.
CE
Am
plifiers.
4.R
C P
hase Shift O
scillator5.
Class A
Pow
er Am
plifier
6.M
icro Processor
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DIII Y
ear B. T
ech. A
E – I sem
esterT
P C
4+1 0 4
(AE
05029) AIR
CR
AF
T P
RO
DU
CT
ION
TE
CH
NO
LO
GY
UN
IT – I
INT
RO
DU
CT
ION
Classification and com
parision (merits and lim
itations) of manufacturing process,
criterion for selection of a processG
eneral principles of various Casting P
rocesses - Sand casting, die-casting,
centrifugal casting, investment casting, shell m
oulding types
UN
IT - II
WE
LD
ING
Principles and equipm
ent used in arc welding, gas w
elding, resistance welding,
thermit w
elding, recent advances in welding technology, S
oldering and brazingtechniques.
UN
IT - III
MA
CH
ININ
G
General principals (w
ith schematic diagram
only) of working and types-lathe, shaper,
milling m
achines, grinding, drilling m/c, C
NC
machining and general principles.
UN
IT - IV
SH
EE
T M
ET
AL
FO
RM
ING
Sheet m
etal operations-shearing, punching, dropstamp form
ing, Advanced m
etalform
ing (super plastic forming and diffusion bonding). B
end correction for bendingin single plane and bi-directional bending. A
utomation in bend form
ing.
UN
IT- V
UN
CO
NV
EN
TIO
NA
L M
AC
HIN
ING
Principles (w
ith schematic diagram
only) of working and applications of abrasive jet
machining, ultrasonic m
achining, electric discharge machining, electro chem
icalm
achining, laser beam/electron beam
/plasma arc m
achining
2005-20062005-2006
27
UN
IT-V
IH
EA
T T
RE
AT
ME
NT
AN
D S
UR
FA
CE
FIN
ISH
ING
Heat treatm
ent of Alum
inium alloys, titanium
alloys, steels, case hardening, Initialstresses and the stress alleviation procedures. C
orrosion prevention, protectivetreatm
ent for aluminium
alloys, steels, anodizing of titanium alloys, organic coating,
and thermal spray coatings. G
rinding and Polishing, T
echnology of surface finish.
UN
IT - V
IIA
IRC
RA
FT
AS
SE
MB
LY
Aircraft T
ooling Concepts, Jigs, fixtures, stages of assem
bly, types and equipment
for riveted joints, bolted joints (only).
UN
IT - V
IIIQ
UA
LIT
Y C
ON
TR
OL
AN
D A
SS
UR
AN
CE
Concepts and definitions of quality, reliability, quality circles, zero defect program
:international standards, six-sigm
a quality.
ND
T A
ND
OT
HE
R IN
SP
EC
TIO
N T
EC
HN
IQU
ES
Dye P
enetrant Test, X
- ray, magnetic particle and ultrasonic testing. A
ccousticholography.
TE
XT
BO
OK
S:
1.“A
ir craft p
rod
uctio
n te
chn
iqu
es” K
esh
u S
.C, G
an
ap
ath
y K.K
., Inte
rline
Publishing H
ouse, Banglore-1993
2.“M
anufacturing Engineering and T
echnology” by Kalpakajam
– Addison W
esley.
RE
FE
RE
NC
ES
:1.
“Production technology”- R
.K. Jain – K
hanna Publishers – 2002.
2.“P
roduction technology”-O.P
.Khanna and lal. M
.Dhanpat rai publications-N
ewD
elhi-19973.
“Production technology” C
hapman W
.A.J. A
rnold publisher-New
Delhi-1994-
4th edition
4.“P
roduction Technology” by H
industan Machine T
ools (HM
T).
5.“W
orkshop Technology” by H
ajrat Choudhary (V
ol I, II & III) – M
edia Publishers
and Prom
oters – 2002.
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DIII Y
ear B. T
ech. A
E – I sem
esterT
P C
4+1 0 4(A
E05250) F
LIG
HT
ME
CH
AN
ICS
– IU
NIT
-IA
ER
OD
YN
AM
IC C
HA
RA
CT
ER
IST
ICS
Airfoils, w
ings and bodies: geometry, nom
enclature. Aerodynam
ic characteristics.E
ffect o
f ge
om
etry, R
eyn
old
s nu
mb
er, M
ach
no
. Me
asu
res o
f ae
rod
yna
mic
performance. P
erformance augm
entation methods.
UN
IT –II
DR
AG
AN
D T
HR
US
T E
VA
LU
AT
ION
SD
rag of aerospace vehicle components. T
otal drag estimation, M
ethods of dragreduction, P
ropellers, Perform
ance analysis. Aerospace engines reciprocating,
turbine and rockets. Design features. P
erformance characteristics.
UN
IT –III
AIR
CR
AF
T P
ER
FO
RM
AN
CE
IN S
TE
AD
Y F
LIG
HT
Level flight, Stall, C
ruise, Maxim
um speed, C
eiling, Cruise clim
b, Range and
endurance. Clim
b performance, P
erformance optim
ization.U
NIT
-IVP
ER
FO
RM
AN
CE
IN A
CC
EL
ER
AT
ED
FL
IGH
TT
ake-off and landing. Level turns and maneuvers.
UN
IT-V
PE
RF
OR
MA
NC
E O
F R
OC
KE
TS
AN
D M
ISS
ILE
SP
rincipal design features of rockets and missiles. T
ypes, Applications, S
taging,Launch and C
limb. P
erformance in boost glide, boost sustain, long range cruise
and long - range ballistic trajectories.U
NIT
-VI
Introduction to Flight path and perform
ance optimizations.
UN
IT-V
IIIntroduction to S
onic boom and hazards of T
ransonic and Supersonic F
light. Flight
path control based on Ground noise considerations.
UN
IT-V
IIIR
igid Body M
echanics relevant to Aircrafts, space crafts and M
issiles.T
EX
T B
OO
KS
1.A
nderson, J .D., A
ircraft Perform
ance and Design, M
c Graw
-Hill International
Edition 1999
2.C
lancy, L.J., Aerodynam
ics, Pitm
an, 1986
RE
FE
RE
NC
ES
:1.
PerP
erkins, C.D
., and Hage, R
.E., A
irplane Perform
ance and Stability and
Control, W
iley Toppan, 1974
2.M
ilne Thom
son, Theoretical A
erodynamics, M
acmillan, 1985
3.H
oughton, E.L., and C
arruthers, N.B
., Aerodynam
ics for Engineering S
tudents,E
dward A
rnold Publishers Ltd., London, 1989
4.C
hin SS
, Missile C
onfiguration Design, M
c Graw
Hill, N
ew Y
ork, 1961.
2005-20062005-2006
28
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DIII Y
ear B. T
ech. A
E – I sem
esterT
P C
4+1 0 4(A
E05017) A
ER
OD
YN
AM
ICS
– IIT
ables/C
od
es: Isentro
pic E
xpan
sion
, No
rmal S
ho
ck, Ob
liqu
e Sh
ock.
UN
IT-I
ON
E D
IME
NS
ION
AL
FL
OW
S
Isentropic process for closed system/flow
processes. Velocity of sound. M
achnum
ber, flow regim
es. Governing equations of inviscid com
pressible flow. C
ontinuity,M
omentum
and Energy equations in Integral and D
ifferential form. S
tagnationconditions.
UN
IT-II
FL
OW
TH
RO
UG
H N
OZ
ZL
ES
Isentropic flow through C
onvergent – Divergent nozzles. C
hocked flow conditions.
Norm
al shock. Under and O
ver expansion conditions. Flow
through diffusers – wave
reflections from a free boundary. D
escription of supersonic wind tunnels and rocket
engine.
UN
IT-III
OB
LIQ
UE
SH
OC
KS
AN
D E
XP
AN
SIO
N W
AV
ES
Oblique shock relations. S
uper sonic flow over a w
edge θ, β, M relations strong
and weak shock solutions / S
hock polar. Regular reflection from
a solidboundary. Intersections of shock w
ave. Expansion w
aves. Prandtl – M
eyerE
xpansion.
UN
IT-IV
SU
BS
ON
IC C
OM
PR
ES
SIB
LE
FL
OW
OV
ER
AIR
FO
IL
Introduction - Velocity potential equation – T
ransonic small perturbation equation -
Prandtl-G
lauert compressibility corrections - C
ritical Mach num
ber - Drag divergence
Mach num
ber - Area rule - S
upercritical airfoil.
UN
IT-V
SU
PE
RS
ON
IC F
LO
W
Linearized supersonic flow- Linearized supersonic flow
over airfoil and wings. S
hockE
xpansion theory. Detached shock. A
xi-symm
etrical flows-flow
past slender bodiesof revolution, conical flow
s-Num
erical integration procedure.
UN
IT-V
IH
YP
ER
SO
NIC
FL
OW
S
Qualitative aspects of hypersonic flow
. New
tonian theory. Flat plate at an angle of
attack. Hypersonic shock w
ave relations. Lift and drag of wings at hypersonic speeds.
Recent advances in hypersonic flow
s and testing techniques.
UN
IT-V
IIF
LO
W M
EA
SU
RE
ME
NT
S A
ND
MO
DE
L T
ES
TIN
G
Non dim
ensional parameters and
II numbers S
imilarity of flow
s. Model testing in
wind tunnels. P
ressure, Velocity m
easurements – H
otwire and Laser – D
oppleranem
ometer, T
urbulence measurem
ents. Measurem
ent errors. Test section speed,
horizontal buoyancy, flow angularities.
UN
IT-V
IIIF
OR
CE
ME
AS
UR
EM
EN
TS
WIN
D T
UN
NE
L B
AL
AN
CE
S
Force m
easurements – W
ind tunnel balances. Scale effects and corrections, w
allinterferences, induced drag and other com
putations/corrections.
TE
XT
BO
OK
S1.
Anderson, J .D
., Fundam
ental of Aerodynam
ics, Mc G
raw-H
ill Internationalthird edition S
ingapore-2001.2.
Radhakrishnan, E
, E., G
as Dynam
ics, Prentice H
all of India, 1995
RF
FE
RE
NC
ES
1.A
nderson, J .D., M
odern Com
pressible Fluid F
low, M
c Graw
-Hill International
Edition
2.H
od
ge
B.K
& K
oe
nig
K C
om
pre
ssible
Flu
id D
yna
mics w
ith C
om
pu
ter
Application, P
rentice Hall, 1995
3.C
lancy, L.J., Aerodynam
ics, Pitm
an, 1986, Macm
illan, 1985
2005-20062005-2006
29
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DIII Y
ear B. T
ech. A
E – I sem
esterT
P C
4+1 0 4(A
E05023) A
ER
OS
PA
CE
VE
HIC
LE
ST
RU
CT
UR
ES
– I
UN
IT - I
ST
AT
ICA
LL
Y D
ET
ER
MIN
AT
E B
EA
MS
Direct solution of G
overning Differential equations for 1-D
continua. McC
auley’sm
ethod and introduction of singularity methods for internal force as w
ell as deflectionanalysis. B
eam of constant strength and com
posite beams.
UN
IT - II
ST
AT
ICA
LL
Y IN
DE
TE
RM
INA
TE
BE
AM
S A
ND
FR
AM
ES
Order of redundancy, Introduction to redundant analysis, statically determ
inatem
odels and introduction of compatibility, principles for redundant analysis, m
atrixm
ethods for redundant analysis of frames.
UN
IT - III
UN
SY
MM
ET
RIC
BE
ND
ING
Stress analysis of isotropic, com
posite beams including unsym
metrical beam
s.
UN
IT - IV
CO
LU
MN
S
Colum
ns with various end conditions, colum
n curves, columns w
ith initial curvature,w
ith eccentric loading, short column form
ulae like Rankine’s, Johnson’s, etc, E
nergym
ethod
UN
IT - V
BE
AM
CO
LU
MN
S
Introduction to beam colum
ns, elementary treatm
ent.
UN
IT - V
I
EN
ER
GY
PR
INC
IPL
ES
AN
D M
ET
HO
DS
Introduction to energy principles and methods, P
VD
& P
VF
, Castigliano’s theorem
,M
axwell’s reciprocal theorem
, Unit load m
ethod. Direct application of energy
principles to beams, trusses, fram
e, rings, etc.
UN
IT – V
II
The displacem
ent method (R
ayleigh Ritz m
ethod) for redundant analysis of 1-Dstructures (rods, shafts and beam
s), Sim
ple illustration for general stress analysis.
UN
IT – V
III
D’A
lembert’s principle and concepts of S
tiffness, Mass G
eometric stiffness. M
atrixevaluation of equilibria for statics, dynam
ics and stability. Derivations of kinem
aticallyconsistent load vectors, Illustration of solutions w
ith simple exam
ples.
TE
XT
BO
OK
S
1.T
imoshenko, S
., “Strength of m
aterials”, Vols. I &
II, Princeton, D
.Von N
ostrandC
o., 1988.
2.D
onaldson, B.K
, “Analysis of A
ircraft Structures – A
n Introduction”, McG
rawH
ill, 1993.
RE
FR
EN
CE
S
1.M
egson TH
G, “A
ircraft Structures for E
ngineering students”, Edw
ard Arnold
Publication.
2.M
ott, “Applied S
trength of materials”, P
HI.
3.B
.C.P
unmia, “T
heory of Structures”, Laxm
i Publication.
4.E
gor P. P
opov, “Engineering M
echanics of Solids” - P
HI
5.S
.Ra
ma
mru
tha
m, R
.Na
raya
na
n, “T
he
ory o
f Stru
cture
s” – D
ha
np
at R
ai
Publishing C
o, 2003.6.
“Strength of M
aterials”, S.R
amam
rutham – D
hanpat Rai
2005-20062005-2006
30
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DIII Y
ear B. T
ech. A
E – I sem
esterT
P C
4+1 0 4(A
E05020) A
ER
OS
PA
CE
PR
OP
UL
SIO
N – I
UN
IT -I
FU
ND
AM
EN
TA
LS
OF
GA
S T
UR
BIN
E E
NG
INE
SIllustration of w
orking of gas turbine engine - The thrust equation - F
actors affectingthrust – E
ffect of pressure, velocity and temperature changes of air entering
compressors – M
ethod of thrust augmentation – C
haracteristics of turboprop, turbojet– P
erformance characteristics.
UN
IT - II
SU
BS
ON
IC IN
LE
TS
Internal flow and S
tall in Subsonic inlets - B
oundary layer separation – Major features
of external flow near a subsonic inlet – R
elation between m
inimum
area ratio andeternal deceleration ratio - D
iffuser performance .
UN
IT - III
SU
PE
RS
ON
IC IN
LE
TS
Supersonic inlets - S
tarting problem in supersonic inlets - S
hock swallow
ing by areavariation- E
xternal deceleration – Modes of inlet operation.
UN
IT - IV
CO
MB
US
TIO
N C
HA
MB
ER
S A
ND
PE
RF
OR
MA
NC
E
Classification of com
bustion chambers – Im
portant factors affecting combustion
chamber design – C
ombustion process – C
ombustion cham
ber performance.
UN
IT - V
PE
RF
OR
MA
NC
E S
EN
SIT
IVIT
Y
Effect of operating variables on perform
ance - Flam
e tube cooling - Flam
e stabilization– U
se of flame holders – N
umerical problem
s.
UN
IT - V
IN
OZ
ZL
ES
Theory of flow
in isentropic nozzles - Convergent nozzles and nozzle choking –
Nozzle throat conditions – N
ozzle efficiency – Losses in nozzles – Over-expanded
and under-expanded nozzles - Ejector and variable area nozzles - Interaction of
nozzle flow w
ith adjacent surfaces – Thrust reversal .
UN
IT - V
IIC
EN
TR
IFU
GA
L C
OM
PR
ES
SO
RS
Principle of operation of centrifugal com
pressors - Work done and pressure rise -
Velocity diagram
s - Diffuser vane design considerations – C
oncept of Prew
hirl –R
otating stall.
UN
IT - V
IIIA
XIA
L F
LO
W C
OM
PR
ES
SO
RS
Elem
entary theory of axial flow com
pressor – Velocity triangles – D
egree of reaction- T
hree dimensional flow
- Air angle distribution for free vortex and constant reaction
designs - Com
pressor blade design - Centrifugal and A
xial compressor perform
ancecharacteristics.
TE
XT
BO
OK
S
1.M
athur M L &
Sharm
a R P
; Gas T
urbines and Jet & R
ocket Propulsion, S
tandardP
ublisher, Delhi, 2000.
2.C
ohen, H. R
ogers, G.F
.C. and S
aravanamuttoo, H
.I.H. G
as Turbine T
heory,Longm
an, ELB
SE
d, 1989.
RE
FE
RE
NC
ES
1.O
ates G C
, AeroT
hermodyanam
ics of Aircraft E
ngine Com
ponents, AIA
A E
dn.S
ervices, NY
, 1986.2.
Rolls- R
oyce, Jet Engine, 3
rd edition, 1983.3.
Ganesan V
, Gas T
urbines, TM
GH
Pub C
o & ed, D
elhi, 1999.4.
Philipa H
ill and Carl P
eterson, Mechanics and T
hermodynam
ics of Propulsion,
Addison W
esley Longman Inc, 1999.
2005-20062005-2006
31
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
III Year B
. Tech
. AE
– I semester
T P
C4+1 0 4
(EE
05149) CO
NT
RO
L S
YS
TE
MS
UN
IT – I IN
TR
OD
UC
TIO
N
Concepts of C
ontrol System
s- Open Loop and closed loop control system
s and
their differences- Different exam
ples of control systems- C
lassification of controlsystem
s, Feed-B
ack Characteristics, E
ffects of feedback.
Mathem
atical models – D
ifferential equations, Impulse R
esponse and transfer
functions - Translational and R
otational mechanical system
s
UN
IT II T
RA
NS
FE
R F
UN
CT
ION
RE
PR
ES
EN
TA
TIO
NT
ransfer Function of D
C S
ervo motor - A
C S
ervo motor- S
ynchro transmitter and
Receiver, B
lock diagram representation of system
s considering electrical systems
as examples -B
lock diagram algebra – R
epresentation by Signal flow
graph -R
eduction using mason’s gain form
ula.
UN
IT-III
TIM
E R
ES
PO
NS
E A
NA
LY
SIS
Standard test signals - T
ime response of first order system
s – Characteristic E
quationof F
eedback control systems, T
ransient response of second order systems - T
ime
domain specifications – S
teady state response - Steady state errors and error
constants – Effects of proportional derivative, proportional integral system
s.
UN
IT – IV
ST
AB
ILIT
Y A
NA
LY
SIS
IN S
-DO
MA
IN
The concept of stability - R
outh stability criterion – qualitative stability and conditional
stability
Ro
ot L
ocu
s Tech
niq
ue:
The root locus concept - construction of root loci-effects of adding poles and zeros
to G(s)H
(s) on the root loci.
UN
IT – V
FR
EQ
UE
NC
Y R
ES
PO
NS
E A
NA
LY
SIS
Introduction, Frequency dom
ain specifications-Bode diagram
s-Determ
ination of
Frequency dom
ain specifications and transfer function from the B
ode Diagram
-Phase
margin and G
ain margin-S
tability Analysis from
Bode P
lots.
UN
IT – V
I ST
AB
ILIT
Y A
NA
LY
SIS
IN F
RE
QU
EN
CY
DO
MA
IN
Polar P
lots, Nyquist P
lots and applications of Nyquist criterion to find the stability –
Effects of adding poles and zeros to G
(s)H(s) on the shape of the N
yquist diagrams.
UN
IT – V
II CL
AS
SIC
AL
CO
NT
RO
L D
ES
IGN
TE
CH
NIQ
UE
S
Com
pensation techniques – Lag, Lead, Lead-Lag Controllers design in frequency
Dom
ain, PID
Controllers.
UN
IT – V
III ST
AT
E S
PA
CE
AN
AL
YS
IS O
F C
ON
TIN
UO
US
SY
ST
EM
S
Concepts of state, state variables and state m
odel, derivation of state models from
block diagrams, D
iagonalization- Solving the T
ime invariant state E
quations- State
Transition M
atrix and it’s Properties
TE
XT
BO
OK
S:
1.C
ontrol System
s Engineering – by I. J. N
agrath and M. G
opal, New
Age
International (P) Lim
ited, Publishers, 2
nd edition.
2.M
odern Control E
ngineering – by Katsuhiko O
gata – Prentice H
all of India Pvt.
Ltd., 3rd edition, 1998.
RE
FE
RE
NC
ES
:
1.C
ontrol System
s by N.K
.Sinha, N
ew A
ge International (P) Lim
ited Publishers,
3rd E
dition, 1998.2.
Autom
atic Control S
ystems 8th edition– by B
. C. K
uo 2003– John wiley and
son’s.3.
Control S
ystems E
ngg. by NIS
E 3
rd Edition – John W
iley
4.“ M
odelling & C
ontrol Of D
ynamic S
ystems” by N
arciso F. M
acia George J.
Thaler, T
homson P
ublishers.
2005-20062005-2006
32
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
III Year B
. Tech
. AE
– I semester
T P
C
0 – 3 – 2
(AE
05028) AIR
CR
AF
T M
AT
ER
IAL
S &
PR
OD
UC
TIO
N L
AB
Exercises in Lathe, S
haper, Milling, S
lotting, ED
M, C
NC
and Grinding m
achines
comprising the follow
ing.
PR
OD
UC
TIO
N L
AB
1.P
lain Turning, T
aper turning, Facing, K
nurling, Thread C
utting.
2.D
rilling, boring, counter boring, counter sinking
3.S
haping and planning of square blocks, V-w
ays and Dovetail w
ays
4.P
lain Milling
5.G
ear Milling
6.C
ylindrical Grinding / S
urface Grinding
7.S
imple exercises in E
DM
8.S
heet metal joining by rivets, S
oldering and brazing.
9.S
imple exercises on C
NC
machines and P
rogramm
e generation.
MA
TE
RIA
LS
LA
B
10.A
ircraft wood gluing practice
11.S
tudy of properties of sandwich structures
12.S
tudy of Micro S
tructures of Non ferrous alloys
13.E
xperiment on A
utoclave for different geometrical structures.
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
III Year B
. Tech
. AE
– I semester
T P
C
0 – 3 – 2
(AE
05018) AE
RO
DY
NA
MIC
S &
PR
OP
UL
SIO
N L
AB
AE
RO
DY
NA
MIC
S L
AB
1.F
luid flow studies using blow
er
2.C
alibration of lowspeed w
ind tunnel
3.D
rag of different bodies
4.P
ressure distribution studies on two-dim
ensional models
5.P
ressure distribution over an airfoil at different angles of attack
6.M
easurements in w
ind tunnel, such as boundary layer measurem
ents, wake
survey etc.
7.A
xial Flow
Com
pressor
8.C
entrifugal Flow
Com
pressor
9.F
low V
isualization Techniques.
PR
OP
UL
SIO
N L
AB
1.S
tudy of piston engine (Valve T
iming A
nd Port T
iming D
iagram)
2.S
tripping of a piston engine, visual inspection and reasoning for comm
on
troubles and trouble shooting
3.P
erformance of piston engine
4.H
eat Balance T
est on piston engine
5.E
ngine Balancing
2005-20062005-2006
33
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DIII Y
ear B. T
ech. A
E – II sem
esterT
P C
4+1 0 4(A
E05251) F
LIG
HT
ME
CH
AN
ICS
- IIU
NIT
– ID
egree of freedom of a system
- Static and dynam
ic stability - Need for stability in an
airplanes - Purpose of controls - Inherently and m
arginally stable airplanes.
UN
IT – II
EQ
UA
TIO
NS
OF
MO
TIO
N
Equations of m
otion of a rigid body. Inertial forces and mom
ents. Equations of m
otionof flight vehicles. A
erodynamic forces and m
oments. D
ecoupling of longitudinal andlateral-directional equations. Linearisation of equations.
UN
IT - III
AE
RO
DY
NA
MIC
ST
AB
ILIT
Y D
ER
IVA
TIV
ES
Ae
rod
yna
mic sta
bility a
nd
con
trol d
eriva
tives. R
ela
tion
to g
eo
me
try, fligh
tconfiguration. E
ffects of power, com
pressibility and flexibility.
UN
IT – IV
ST
AT
IC L
ON
GIT
UD
INA
L S
TA
BIL
ITY
AN
D C
ON
TR
OL
– CO
NT
RO
L F
IXE
D
Stick F
ixed: Basic equilibrium
equation - Stability criterion – C
ontribution of wing and
tail and elevator to pitching mom
ents - Effect of fuselage and nacelles - E
ffects ofcenter of gravity location - P
ower effects - S
tabiliser setting and center of gravitylocation – E
levator power– E
levator to trim . T
rim gradients. C
ontrol fixed staticstability – C
ontrol fixed neutral point. Stability m
argins.
UN
IT – V
ST
AT
IC L
ON
GIT
UD
INA
L S
TA
BIL
ITY
– CO
NT
RO
L F
RE
E
Effects of releasing the elevator. H
inge mom
ent coefficients – Control forces to trim
.C
ontrol free neutral point – Trim
tabs. Aerodynam
ic balancing of control surfaces.M
eans of augmentation of control.
UN
IT – V
IM
AN
EU
VE
R S
TA
BIL
ITY
Contribution of pitch dam
ping to pitching mom
ent of flight vehicle - Effect on trim
andstability. C
ontrol deflections and control forces for trim in sym
metric m
aneuvers andcoordinated turns. C
ontrol deflection and force gradients. Control fixed and control
free maneuver stability. M
aneuver points. Maneuver m
argins.
UN
IT – V
IIS
TA
TIC
LA
TE
RA
L A
ND
DIR
EC
TIO
NA
L S
TA
BIL
ITY
AN
D C
ON
TR
OL
Dihedral effect - C
oupling between rolling and yaw
ing mom
ent - Adverse yaw
-A
ileron power - A
ileron reversal. Weather cocking effects – R
udder power. Lateral
and directional stability- definition. Control surface deflections in steady sideslips,
rolls and turns one engine inoperative conditions - Rudder lock.
UN
IT – V
IIID
YN
AM
IC S
TA
BIL
ITY
AN
D R
ES
PO
NS
E T
O C
ON
TR
OL
.
Solutions to the stability quartic of the linearised equations of m
otion. The principal
modes. P
hugoid , Short P
eriod Dutch R
oll and Spiral m
odes - Further approxim
ations.R
estricted degrees of motion. S
olutions. Response to controls. A
uto rotation andspin.
TE
XT
BO
OK
S
1.H
oughton, E.L., and C
arruthers, N.B
., Aerodynam
ics for Engineering S
tudents,E
dward A
rnold Publishers Ltd., London, 1989
2.M
c.Corm
ic, B.W
., Aerodynam
ics, Aeronautics &
Flight M
echanics, John Wiley
1995
RE
FE
RE
NC
ES
1.P
erkins C.D
., & H
age, R.E
., Airplane P
erformance, S
tability and Control, W
ileyT
oppan 1974.
2.N
elson, R.C
., Flight S
tability and Autom
atic Control, M
cGraw
Hill 1989
2005-20062005-2006
34
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DIII Y
ear B. T
ech. A
E – II sem
esterT
P C
4+1 0 4
(AE
05024) AE
RO
SP
AC
E V
EH
ICL
E S
TR
UC
TU
RE
S – II
UN
IT – I
LO
AD
DIF
FIS
ION
IN S
TIF
FN
ED
PA
NE
LS
Wagner’s theory of beam
s. Shear carrying capabilities of panels and introduction to
Tension field w
ebs. Sem
i tension and full tension field beams. M
onocoque andsem
i Monocoque structures.
UN
IT – II
Axial Load flow
diagrams for boom
in stiffened panels. Sim
ple illustrate examples of
A/C
sheet stringer elements through F
ree body diagrams.
UN
IT – III
Load diffusion in thin walled panels w
ith oblique stiffness (at right angles to thebottom
).
UN
IT – IV
Stability of stiffened panels. E
ffective width concept. S
imple estim
ations of loadcarrying capability of stressed skins.
UN
IT – V
SH
EA
R F
LO
W IN
OP
EN
SE
CT
ION
S
Thin w
alled beams - C
oncept of shear flow - S
hear centre - Elastic axis of box
beams w
ith one axis of symm
etry, Unsym
metrical box beam
with effective and
ineffective skins.
UN
IT - V
IS
HE
AR
FL
OW
IN C
LO
SE
D S
EC
TIO
NS
Bredt-B
atho formula. S
ingle and multi-cell closed box structures. A
pproximate m
ethodbox beam
s. Shear flow
in single & m
ulticell structures beams torsion. S
hear flow in
single and multicell m
onocoque and semi m
onocoque box beams.
UN
IT - V
IIS
TR
ES
S A
NA
LY
SIS
OF
WIN
G A
ND
FU
SE
LA
GE
Procedure - S
hear and bending mom
ent distribution for semi cantilever and other
types of wings and fuselages - T
hin webbed beam
with parallel and non parallel
flanges - Shear resistant w
eb beams.
UN
IT-V
IIIIN
TR
OD
UC
TIO
N T
O F
AT
IGU
ER
epetitive loads, Endurance strength, stress concentration factor, S
-N curve,
Goodm
an &S
oderberg lines, low cycles and high cycle fatigue, cum
ulative fatiguedam
age for multiple stress cycles-M
iner’s rule
TE
XT
BO
OK
S
1.M
egson, T.M
.G., A
ircraft Structures for E
ngineering Students, E
dward A
rnold,
1985.2.
J.T. O
den, “Mechanics of E
lastic Structures”, M
cGraw
-Hill.
RE
FE
RE
NC
ES
1.P
eery, D.J, and A
zar, J.J., Aircraft S
tructures, 2nd edition, Mc G
raw-H
ill, N.Y
.,
1993.2.
Rivello, R
.M., T
heory and Analysis of F
light Structures, M
cGraw
Hill, 1993.
3.B
ruhn. E.H
, Analysis and D
esign of Flight V
ehicles Structures, tri -state off set
company, U
SA
, 1965.
4.K
uhn.P, “S
tresses in Aircraft and S
hell Structure”, M
cGraw
-Hill.
5.W
illiam.D
, “An Introduction to the T
heory of Aircraft S
tructures”, Edw
ard Arnold.
6.S
cheler.E.E
and Dunn L.G
, “Airplane S
tructural Analysis and D
esign”, John
Wiley &
Sons.
7.K
ermode.A
.C, “T
he Airplane S
tructure”, Sir Issacc P
itman P
ublication.
8.D
owty G
.H, “S
tructural Principles and D
ata”, The new
ER
A P
ublishing Cp,
1980.9.
“Mechanical E
ngineering Design” by Joseph. E
. Shigley and C
harless R.
Mischeke, T
MH
-2003.10.
Machine D
esign by Pandy and S
ha, Charotar P
ublishing house- 1997.
2005-20062005-2006
35
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
III Year B
. Tech
. AE
– II semester
T P
C4+1 0 4
(AE
05021) AE
RO
SP
AC
E P
RO
PU
LS
ION
– II
UN
IT - I
GA
S T
UR
BIN
E T
HE
OR
IES
Impulse and reaction blading of gas turbines - V
elocity triangles and power output -
Elem
entary theory - Vortex theory - C
hoice of blade profile, pitch and chord -E
stimation of stage perform
ance.
UN
IT – II
DE
SIG
N C
ON
SIL
RE
TIO
NS
Limiting factors in gas turbine design - O
verall turbine performance - M
ethods ofblade cooling - M
atching of turbine and compressor - N
umerical problem
s.
UN
IT – III
TH
RU
ST
CO
NT
RO
L
Thrust A
ugmentation through after burning, thrust vector control m
ethods.
UN
IT – IV
RA
MJE
T P
RO
PU
LS
ION
Operating principle- S
ubcritical, critical and supercritical operation - Com
bustion inram
jet engine - Ram
jet performance - S
ample ram
jet design calculations - Introductionto S
CR
AM
JET
- Prelim
inary concepts in supersonic combustion - Integral ram
-R
ocket - Num
erical problems.
UN
IT - V
FU
ND
AM
EN
TA
LS
OF
RO
CK
ET
PR
OP
UL
SIO
N
Operating principle - S
pecific impulse of a rocket - Internal ballistics - R
ocket nozzleclassifications - R
ocket performance considerations - N
umerical problem
s.
UN
IT - V
IC
HE
MIC
AL
RO
CK
ET
S
Solid propellant rockets - S
election criteria of solid propellants - Important hardw
arecom
ponents of solid rockets – Propellant grain design considerations.
UN
IT - V
II
Liquid propellant rockets - Cooling in liquid rockets - Lim
itations of hybrid rockets -R
elative advantages of liquid rockets over solid rockets.
UN
IT - V
IIIA
DV
AN
CE
D P
RO
PU
LS
ION
TE
CH
NIQ
UE
S
Electric rocket propulsion - Ion propulsion techniques - N
uclear rocket - Types -
Solar sail- P
reliminary concepts in nozzle less propulsion.
TE
XT
BO
OK
S
1.S
utton, G.P
., Rocket P
ropulsion Elem
ents, John Wiley &
Sons Inc., N
ew Y
ork,
5th Ed., 1993.
2.P
hilipa Hill and C
arl Peterson, M
echanics and Therm
odynamics of P
ropulsion,
Addison W
esley Longman Inc, 1999.
RE
FE
RE
NC
ES
1.M
arcl Bacare et. al. R
ocket Propulsion, E
lsevier Pub C
o, 1960.
2.Z
ucrow M
J, Aircraft &
Missile P
ropulsion, John Wiley &
Sons, N
Y, 1964.
3.G
orden, C.V
., Aerotherm
odynamics of gas turbine and R
ocket Propulsion, A
IAA
Education S
eries, New
York, 1986.
4.O
ates G C
, AeroT
hermodyanam
ics of Aircraft E
ngine Com
ponents, AIA
A E
dn.
Services, N
Y, 1986.
5.R
olls- Royce, Jet E
ngine, 3rd edition, 1983.
6.C
ohen. H., R
ogers, G.F
.C. and S
aravanamuttoo, H
.I.H., G
as turbine theory,
Longman C
o., ELB
S E
d., 1989.
7.G
anesan V, G
as Turbines, T
MG
H P
ub Co &
ed, Delhi, 1999.
8.M
athur, M., and S
harma, R
.P., G
as Turbines and Jet and R
ocket Propulsion,
Standard P
ublishers, New
Delhi, 1988.
9.S
M Y
ahya, Fundam
entals of Com
pressible Flow
with A
ircraft and Rocket
propulsion, New
Age International P
ub, Delhi, 2003.
2005-20062005-2006
36
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DIII Y
ear B. T
ech. A
E – II sem
esterT
P C
4+1 0 4(A
E05132) C
OM
PU
TA
TIO
NA
L A
ER
OD
YN
AM
ICS
UN
IT-I - B
AS
ICS
Introduction to computational fluid dynam
ics – Research tool – D
esign Tool, F
initecontrol volum
e, infinitesimal fluid elem
ent, substantial derivatives, divergence ofV
elocity.
UN
IT-II - G
OV
ER
NIN
G E
QU
AT
ION
S O
F F
LU
ID D
YN
AM
ICS
The continuity equation, the m
omentum
equation, the energy equation, physicalboundary conditions.
UN
IT-III - S
HO
CK
FIT
TIN
G A
ND
SH
OC
K C
AP
TU
RIN
G
Form
of Governing equation suited for C
FD
- Conservation form
- shock fitting andshock capturing.
UN
IT-IV
- IMP
AC
T O
F P
AR
TIA
L D
IFF
ER
EN
TIA
L E
QA
UT
ION
S O
N C
FD
Introduction, Classification of Q
uasi-Linear Partial differential equation, T
he Eigen
value method, G
eneral behavior of different classes of Partial differential equation –
elliptic, parabolic and hyperbolic.
UN
IT-V
- DIS
CR
ET
IZA
TIO
N
Introduction, Finite differences, difference equations, E
xplicit and implicit approaches,
Errors and an analysis of stability.
UN
IT-V
I - TR
AN
SF
OR
MA
TIO
NS
Introduction, transformation of the governing partial differential equations, M
atricesand the Jacobian of transform
ation
UN
IT-V
II - GR
ID G
EN
ER
AT
ION
S – I
Grid G
eneration techniques, Elliptic G
rid Generator – S
imply connected dom
ain –doubly connected dom
ain.
UN
IT-V
III - GR
ID G
EN
ER
AT
ION
S – II
Coordinate system
control – Grid P
oint clustering, Introduction to Hyperbolic G
ridG
eneration techniques and parabolic grid generator.
TE
XT
BO
OK
S
1.H
offmann, K
.A: C
omputational F
luid Dynam
ics for Engineers, E
ngineeringE
ducation System
, Austin, T
ex., 1989
2.K
reyszig,E., A
dvanced Engineering M
athematics, W
iley, New
York
RE
FE
RE
NC
ES
1.John .D
. Anderson “ C
omputational F
luid Dynam
ics”, McG
raw H
ill
2.A
nderson, Dale A
., John C. T
anhill and Richard H
. Pletcher, “C
omputational
Flu
id M
ech
an
ics an
d H
ea
t Tra
nsfe
r”, McG
raw
Hill, N
ew
Yo
rk 19
84
,V
olumes I &
II
3.Introduction to C
omputational F
luid Dynam
ics, Chow
CY
, John Wiley, 1979
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
III Year B
. Tech
. AE
– II semester
T P
C4+1 0 4
(AE
05247) FIN
ITE
EL
EM
EN
T A
ND
MO
DE
LL
ING
ME
TH
OD
S
UN
IT – I
MO
DE
LS
Macro and M
icro mechanical m
odels and ‘The F
inite Elem
ents’-Bases of developing
and specification structural models. E
quilibrium and energy bases for designing
such as stiffness, flexibility, Inertia, damping and stability characteristics. D
egreesof freedom
and their relevance’s to approximate m
ethods of analysis
UN
IT – II
GE
NE
RE
LIZ
ED
CO
OR
DIN
AT
ES
Introduction to generalized coordinates and their classification based frames of
reference (local/global), nature and utility. Field specific nature of such coordinates
in time &
space for representing both continuua and discontinuua. Nom
dimensional
coordinates, Area and V
olume coordinates, utility of generalized coordinates in
respresenting continuum and discrete system
s.
UN
IT – III
DIS
CR
ET
IZA
TIO
N
Role of interpolation (H
ermitian and Langragian) functions in discretization – concepts
of nodes and elements in discretizing 1 – D
and 2 – D S
olid fluid continuua. Exam
plesof discretization of heat conduction, shear, axial, T
orsional and Bending deform
ationsof constant and stepped – 1-D
structures. Discretization of plane stress P
lain strainand 3-D
space frame problem
s
UN
IT – IV
PR
OP
ER
TIE
S A
ND
DE
RIV
AT
ION
Derivation of elem
ent property matrices from
first principles - energy basis for derivingstiffness, m
ass element properties – A
ssembly T
echnique - Concept of w
ork doneand derivation of kinem
atically consistent load vectorsD
irect deduction of matrix equation of equilibria using assem
bly technique for propertyderivation for 1-D
structures and frames.
2005-20062005-2006
37
UN
IT – V
AP
PR
OX
IMA
TIO
NS
AN
D E
RR
OR
CO
NT
RO
L
Nodal param
etric representation of discrete domains and fields. Isoparam
etric,S
ubparametric and S
uperparametric representation. Injection of singularity in field
distortions and their utility in fracture mechanics.
UN
IT – V
IM
AT
HE
MA
TIC
AL
TO
OL
S A
ND
FE
M T
OO
LS
Importance of designing codes in discretizing. Illustration of 1-D
and 2-D field
problems. B
asics of Num
erical integration and Gauss quadrature. T
echniques ofdata storage and solution of storage of large scale m
atrices. Concept of bandw
idthand F
ront widths and their m
inimization. In core, and out of core solution of based
on matrices. F
rontal techniques.
UN
IT – V
II
Sym
metries in F
ields. 1 – dimensional, 2 A
xial, Polar sym
metry (cyclic), A
xisymm
etryproblem
, symm
etry condition and samplification.
UN
IT – V
III
Mess generation T
echniques, uses of Educational sofw
ares such as Ansys, N
ISA
,N
AS
TR
AN
, AS
KA
, CA
EF
EM
etc.
TE
XT
BO
OK
S
1.C
oncepts and Application of F
EA
, R.D
.Cook, D
avid S. M
ALK
US
, Micheal
E_P
LES
HA
, Robert J. W
itt Wiley S
tudent Edition, India, 2002.
2.S
S R
ao, “The F
inite Elem
ent Methods in E
ngineering”, Pergam
on.
RE
FE
RE
NC
ES
1.S
egarlind, L.J., Applied F
inite Elem
ent Analysis, John W
iley and Sons, Inc.,
New
York, 1991.
2.D
esai, C.S
and Abel, J.F
., An introduction to the F
inite Elem
ent Method, A
ffiliatedE
ast-West P
ress Pvt., Ltd., N
ew D
elhi, 1987.3.
Bathe, K
.J. And W
ilson, E.L., N
umerical M
ethods in Finite E
lement A
nalysis,P
rentice Hall of India, 1985.
4.T
irupathi R.C
handrupatla and Ashok D
Belagundu, “Introduction to F
initeE
lements in E
ngineering”, PH
I5.
“Finite E
lement and M
odelling Methods”, K
SR
K P
rasad.
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
III Year B
. Tech
. AE
– II semester
T P
C4+1 0 4
(AE
05335) INT
RO
DU
CT
ION
TO
SP
AC
E T
EC
HN
OL
OG
Y
UN
IT-I
INT
RO
DU
CT
ION
Space M
ission-Types-S
pace Environm
ent-Launch Vehicle S
election
UN
IT II
FU
ND
AM
EN
TA
LS
OF
RO
CK
ET
PR
OP
UL
SIO
N
Intro
du
ction
to ro
cket p
rop
ulsio
n-fu
nd
am
en
tals o
f solid
pro
pe
llan
t rocke
ts-F
undamentals of liquid propellant rockets-R
ocket equation
UN
IT-III
AS
CE
NT
FL
IGH
T M
EC
HA
NIC
S O
F R
OC
KE
TS
AN
D M
ISS
ILE
S
Tw
o-dimensional trajectories of rockets and m
issiles-Multi-stage rockets-V
ehiclesizing-T
wo stage M
ulti-stage Rockets-T
rade-off Ratios-S
ingle Stage to O
rbit-S
ou
nd
ing
Ro
cket-A
ero
spa
ce P
lan
e-G
ravity T
urn
Tra
jecto
ries-Im
pa
ct po
int
calculation-Injection conditions-Flight dispersions
UN
IT-IV
AT
MO
SP
HE
RIC
RE
EN
TR
Y
Introduction-Steep B
allistic Reentry-B
allistic Orbital R
eentry-Skip R
eentry-“Double-
Dip” R
eentry - Aero-braking - Lifting B
ody Reentry
UN
IT-V
FU
ND
AM
EN
TA
LS
OF
OR
BIT
AL
ME
CH
AN
ICS
Tw
o-body motion-C
ircular, elliptic, hyperbolic, and parabolic orbits-Basic O
rbitalE
lements-G
round Trace
UN
IT-V
IO
RB
ITA
L M
AN
EU
VE
RS
In-Plane O
rbit changes-Hohm
ann Transfer-B
ielliptical Transfer-P
lane Changes-
Com
bined Maneuvers-P
ropulsion for Maneuvers
2005-20062005-2006
38
UN
IT -V
IIS
AT
EL
LIT
E A
TT
ITU
DE
DY
NA
MIC
S
Torque free A
xi-symm
etric rigid body-Attitude C
ontrol for Spinning S
pacecraft -A
ttitude Control for N
on-spinning Spacecraft - T
he Yo-Y
o Mechanism
– Gravity –
Gradient S
atellite-Dual S
pin Spacecraft-A
ttitude Determ
ination
UN
IT-V
IIIS
PA
CE
CR
AF
T P
OW
ER
AN
D C
OM
MU
NIC
AT
ION
SY
ST
EM
S
Spacecraft P
ower-T
elecomm
unications
TE
XT
BO
OK
S
1.“S
paceflight Dynam
ics”, W.E
. Wiesel, M
cGraw
-Hill, 1997
2. “R
ocket Propulsion and S
pace flight dynamics”, C
ornelisse, Schoyer H
FR
,and W
akker KF
, Pitm
an, 1984
RE
FE
RE
NC
ES
1.”U
nderstanding Space: A
n Introduction to Astronautics”, J.S
ellers, McG
raw-
Hill, 2000
2.”Introduction to S
pace Flight”, F
rancis J Hale, P
rentice-Hall, 1994
3.”S
pacecraft Mission D
esign”, Charles D
.Brow
n, AIA
A E
ducation Series, 1998
4.”S
pacecraft Mission D
esign”, Charles D
.Brow
n, AIA
A E
ducation Series, 1998
5.”E
lements of S
pace Technology for A
erospace Engineers”, M
eyer Rudolph X
,A
cademic P
ress, 1999
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
III Year B
. Tech
. AE
– II semester
T P
C0 – 3 – 2
(AE
05022) AE
RO
SP
AC
E S
TR
UC
TU
RE
S L
AB
1.T
ensile testing using universal Testing M
achine - Mechanical and optical
Extensom
eters - Stress - strain curves and strength tests for various engineering
materials.
2.B
ending tests - Stress and deflection of beam
s for various end conditions -
Verification of M
axwell’s and C
astiglianos theorems - Influence coefficients.
3.C
ompression tests on load and short colum
n - Critical buckling loads - S
outh
well plot.
4.T
est on riveted and bolted joints.
5.T
est using ND
T inspection m
ethod.
6.S
train gauge techniques - Measurem
ent of strain in beams, thin and thick w
alled
cylinders subjected to internal pressure - Shaft subjected to com
bined loading.
7.S
hear centre in open and closed sections beams - T
est on semi-tension field
beams.
8.E
lastic constants for composite m
aterials - Flexural test on com
posites.
9.S
tudy and calibration of photo and magnetic speed pickups for the m
easurement
of speed.
10.S
tudy and use of a Seism
ic pickup for the measurem
ent of vibration amplitude.
2005-20062005-2006
39
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
III Year B
. Tech
. AE
– II semester
T P
C0 – 3 – 2
(AE05135) COM
PUTATIONAL STRUCTURAL AND AERO
DYNAMIC ANALYSIS
A.
FIN
ITE
EL
EM
EN
TS
ME
TH
OD
LA
B
UN
IT-I
One of the follow
ing a) E
xercises on discretization b) G
rid generation and element/node num
beringU
NIT
-IIE
lement G
eneration Exercises (tw
o of the following)
1-D elem
ents(rods, shafts and beams)
Plane S
tress /Plane S
train Quadrilateral elem
entsT
riangular plate elements
UN
IT-III
FE
M S
olutions using any one of the following
MA
TLA
BA
NS
YS
NA
ST
RA
NP
RO
- E A
ny one of the normal procedures:
a) Gauss Q
uadrature for unit 1 and 2-D dom
es b) G
eneration of stiffness and load vector matrices.
c) Use of eigen value solvers for frequency and m
ode shapes determination
B. C
FD
LA
B
UN
IT – I
Num
erical solutions for any one of the following, using F
inite difference method.
Elliptic E
quationsP
arabolic Equations
Hyperbolic E
quationsU
NIT
– IIG
rid Generations for any one of the follow
ingA
lgebraically stretched Cartesian grids.
Elliptic grids
UN
IT – III
Num
erical solutions for any one of the following
Vortex panel m
ethodS
ource panel method
Incompressible coutte flow
Supersonic flow
over a flat plate
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
IV Y
ear B. T
ech. A
E – I sem
esterT
P C
4+1 0 4
(AE
05546) TH
EO
RY
OF
VIB
RA
TIO
NS
AN
D A
ER
OE
LA
ST
ICIT
Y
UN
IT - I
INT
RO
DU
CT
ION
Sim
ple Harm
onic Motion, T
erminology, N
ewton’s Law
, D’A
lembert’s P
rinciple,R
eso
nce
, intro
du
ction
to m
ech
an
ism o
f da
mp
ing
. Da
mp
ed
an
d u
nd
am
pe
doscillations.
UN
IT - II
SIN
GL
E D
EG
RE
E O
F F
RE
ED
OM
SY
ST
EM
S
Free vibrations, F
ree damped vibrations, F
orced vibration with and w
ithout damping,
Support excitation, and V
ibration-measuring instrum
ents. Am
plitude and phaseresponse diagram
s
UN
IT – III
MU
LT
I-DE
GR
EE
OF
FR
EE
DO
M S
YS
TE
MS
Tw
o degree of freedom system
s, Static and dynam
ic couplings, Vibration absorber,
Principal coordinates, P
rincipal modes, orthogonality conditions. H
amilton’s principle,
Lagrangean equation and applications. Longitudinal vibration, Lateral vibration,T
orsional vibration of shafts dynamical equations of equilibria of elastic bodies,
natural frequencies and mode shapes determ
ination.
UN
IT - IV
Vibrations of solid continuua. D
etermination of E
igen values and Eigen vectors.
UN
IT – V
GE
NE
RL
IZE
D S
ING
LE
DO
F S
YS
TE
M
Derivation of equations of equilibria stiffness m
ass and damping param
eters forcontinuous system
s for one-D approxim
ation.
UN
IT – V
I
Natural frequency of rotating shafts and w
hirling of shafts. Dynam
ic balancing ofrotating shafts. D
ynamic dam
pers.
2005-20062005-2006
40
UN
IT - V
II
Approxim
ate methods to determ
ine the natural frequencies. Introduction to normal
mode m
ethod of response.
UN
IT - V
III
Collar’s triangle, introduction to A
ero-elasticity, couplings, Aeroelatic instabilities and
their prevention. Static and dynam
ic aero elastic phenomenon W
ing divergence,C
ontrol reversal and Control flutter speed, F
lutter prevention. Aero elastic tailoring.
TE
XT
BO
OK
S:
1.B
isplinghott, R.l., A
shley, H. and H
ogman, R
.l., Aero elasticity, A
ddison Wisely
Publication, N
ew Y
ork, 19832.
Rao, J.S
and Gupta .K
., Theory and practice of M
echanical vibrations, Wiley
Eastern Ltd., N
ew D
elhi, 2002.
RE
FE
RE
NC
ES
:
1.F
ug, Y.C
., An Introduction to T
heory of Aeroelasticity, John W
iley & S
ons, New
York, 1984
2.T
imoshenko, S
., Vibration P
roblems in E
ngineering, John Wiley and S
ons,N
ew Y
ork, 1987.3.
R.W
. Clough and P
enzien, “Dynam
ics of Structures”.
4.S
hock and Vibrations by H
arris & C
reed Mc-G
raw H
ill book company, third
edition.5.
Mechanical V
ibrations by V.P
.Singh, D
hanapati Rai and C
o. 2003 edition.6.
Mechanical V
ibrations by S.G
rahamkelly- T
MH
2004 edition.7.
Mechanical V
ibrations G.K
.Groover, N
emchand and B
rothers 2001 edition.8.
Mechanical V
ibrations by Singiresure.S
.Rao, P
earson Education LP
E-2004.
9.V
ibrations and waves C
BS
Publishers and D
istributors MIT
series 1987.10.
Scanlon, R
.H., &
Rosenbaum
, R., “Introduction to the S
tudy of Aircraft V
ibration&
Flutter.” John W
iley and Sons, N
ew Y
ork, 1982
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
IV Y
ear B. T
ech. A
E – I sem
esterT
P C
4+1 0 4(A
E05252) F
LIG
HT
VE
HIC
LE
DE
SIG
N
UN
IT-I
OB
JEC
TIV
ES
RE
QU
IRE
ME
NT
S O
F T
HE
VE
HIC
LE
: Type, role, m
ission. Payload,
performance and other requirem
ents. Study of com
parable aircraft - principal designand constructional and perform
ance. Data collection and statistical analysis.
UN
IT-II
CO
NC
EP
TU
AL
SK
ET
CH
AN
D F
IRS
T E
ST
IMA
TE
OF
WE
IGH
T : C
onceptual sketchof candidate design- alternative configurations. F
irst estimate of take off w
eight.
UN
IT-III
INIT
IAL
SIZ
ING
: Airfoil and w
ing geometry selection. E
stimate of thrust to w
eightratio and w
ing loading.
UN
IT-IV
FU
SE
LA
GE
AN
D C
ON
TR
OL
SU
RF
AC
ES
: Sizing of F
uselage and control surfaces.
UN
IT-V
CO
NF
IGU
RA
TIO
N L
AY
OU
T : Layout and draw
ing of the configuration. Weight
balance
UN
IT-V
IP
ER
FO
RM
AN
CE
AN
D S
TA
BIL
ITY
ES
TIM
AT
E : P
erformance and stability estim
ate.
UN
IT-V
IIL
OA
D E
ST
IMA
TE
S : A
irload distribution on the wing. P
reliminary structural Layout.
UN
IT-V
IIIR
EV
IEW
: Review
and evaluation of the design.
TE
XT
BO
OK
S1.
Raym
er, Daniel P
. Aircraft D
esign: A C
onceptual Approach (T
hird Edition) A
IAA
Educational S
eries. AIA
A 1999
RE
FE
RE
NC
E1.
Torenbeek E
. Synthesis of S
ubsonic Airplane D
esign. Delft U
niversity Press
1986
2005-20062005-2006
41
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
IV Y
ear B. T
ech. A
E – I sem
esterT
P C
4+1 0 4
(AE
05531) ST
RU
CT
UR
AL
AN
AL
YS
IS A
ND
DE
TA
ILE
D D
ES
IGN
UN
IT – I
LA
ND
ING
GE
AR
Reactions and loads on m
embers of landing gear, oleo strut, torque link
UN
IT – II
FU
SA
LA
GE
– I
Loads, effective cross-section, bending strength, shear flow analysis,
UN
IT – III
FU
SA
LA
GE
– II
Pressurization stresses secondary stresses in stringers, ultim
ate strength of stiffenedcylindrical structures
UN
IT IV
MO
NO
CO
QU
E C
YL
IND
ER
S – I
Strength under pure torsion, external pressure, internal pressure.
UN
IT – V
MO
NO
CO
QU
E C
YL
IND
ER
S – II
Strength under C
ompression, bending and com
bination of them in m
onocoque
cylinders.
UN
IT – V
IW
ING
S-I
Sem
i tension field design, elementary approxim
ate formulae, general W
agnerequations.
UN
IT – V
IIW
ING
S-II
Beam
s with non parallel flanges, engineering theory of incom
plete critical shearstress, loading ratio.
UN
IT – V
IIIF
AIL
SA
FE
DE
SIG
N
Crack propagation, residual strength, fail safe design criterion
TE
XT
BO
OK
S
1.P
eery, D.J, and A
zar, J.J., Aircraft S
tructures, 2nd edition, Mc G
raw-H
ill, N.Y
.,1993.
2.R
ivello, R.M
., Theory and A
nalysis of Flight S
tructures, McG
raw H
ill, 1993.
RE
FE
RE
NC
ES
1.M
egson, T.M
.G., A
ircraft Structures for E
ngineering Students, E
dward A
rnold,1985.
2.B
ruhn. E.H
, Analysis and D
esign of Flight V
ehicles Structures, tri -state off set
company, U
SA
, 1965. J.T. O
den, “Mechanics of E
lastic Structures”, M
cGraw
Hill.
3.K
uhn.P, “S
tressess in Aircraft and S
hell Structure”, M
cGraw
Hill.
4.W
illiam.D
, “An Introduction to the T
heory of Aircraft S
tructures”, Edw
ard Arnold.
5.S
cheler.E.E
and Dunn L.G
, “Airplane S
tructural Analysis and D
esign”, John
Wiley &
Sons.
6.K
ermode.A
.C, “T
he Airplane S
tructure”, Sir Issacc P
itman P
ublication.7.
Dow
ty G.H
, “Structural P
rinciples and Data”, T
he new E
RA
Publishing C
p,
1980.
8.S
higley JE, “M
echanical Engineering D
esign”.9.
Pandya &
Shah, “M
achine Design”
2005-20062005-2006
42
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
IV Y
ear B. T
ech. A
E – I sem
esterT
P C
4+1 0 4
(AE
05027) AIR
CR
AF
T M
AT
ER
IAL
S A
ND
CO
MP
OS
ITE
S
UN
IT- I
Mechanical behavior of engineering m
aterials, liner and non linear elastic properties,yielding, strain hardening, fracture, B
auschinger’s effect, notch effect, testing andflaw
detection of material
UN
IT- II
Introduction, wrought alum
inium alloys, cast alum
inium alloys, production of sem
i-fabricated form
s, aerospace applications
UN
IT -III
INT
RO
DU
CT
ION
TO
CO
MP
OS
ITE
S
Classification, C
haracterization, advantages and applications of composite m
aterials,and structures. S
tructural composites. R
einforcements and m
atrices. Single layer/
multiplayer; sym
metric/unsym
metric and anti-sym
metric lay-up configuration w
ithcross ply and angle ply lay-ups. Introduction 3-D
composites and W
oven composites.
UN
IT -IV
CH
AR
AT
ER
IZA
TIO
N O
F C
OM
PO
SIT
ES
Stress strain relations of com
posites, orthographic behavior of composites, m
echanicsof m
aterials approach to determine young m
odulus, shear modulus and poisson’s
ratio, stress strain relations in material coordinates: strength concepts, B
iaxial strengththeories- m
aximum
stress, maxim
um strain fracture toughness of com
posites.
UN
IT- V
MIC
RO
ME
CH
AN
ICS
OF
CO
MP
OS
ITE
S
Limitation of C
CA
models and introduction to m
icro mechanics. E
lasticity basedm
icro mechanical m
odels. Introduction to of FE
M in com
posite characterization.
UN
IT- V
IF
AB
RIC
AT
ION
PR
OC
ES
SE
S
Open and closed m
ould process, filament w
inding pull- trusion and on-line productionm
ethods of manufacture of fibers and properties
UN
IT -V
IID
AM
AG
E T
OL
ER
AN
CE
Introduction to impact dam
age of composites. Life prediction and dam
age tllarancestudies, fracture toughness of com
posites, ND
T techniques for quality assurance.
UN
IT- V
IIIS
EL
EC
TIO
N O
F M
AT
ER
IAL
S
Environm
ental and manufacturing considerations in selection of m
aterials for aircraftsand rockets. M
aterials used for aircraft components: application of com
positem
aterials, super alloys.
TE
XT
BO
OK
S
1.B
alram G
upta, Aerospace M
aterials Vol. I to V
, S.C
hand & C
ompany Ltd.,
New
Delhi – 1996.
2.“A
nalysis and Perform
ance of fibre Com
posites”, Agarw
al BD
and Broutm
anLJ., John W
iley and Sons., N
Y, 1980.
RE
FE
RE
NC
ES
1.“M
echanics of Com
posite Materials”, Jones R
M., M
cGraw
Hill, K
ogakusha Ltd.,T
okyo, 1985.2.
Titterton, G
., Aircraft M
aterials and Processes, V
Edition, P
itman P
ublishingC
o., 1995.3.
Cindy F
oreman, A
dvanced Com
posites.4.
Lubin G, H
and Book of A
dvanced Plastics and F
ibber glass Von N
arstandR
eihold Co.N
.Y.1989.
5.“H
andbook on Advanced P
lastics and Fibre G
lass:, Lubin G., V
on Nostrand
Reinhold C
o., NY
, 1989.6.
“Advanced C
omposite M
aterials”, Lalit Gupta, H
imalayan B
ooks, New
Delhi,
1998.
2005-20062005-2006
43
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
IV Y
ear B. T
ech. A
E – I sem
esterT
P C
4+1 0 4
(AE
05242) EX
PE
RIM
EN
TA
L S
TR
ES
S A
NA
LY
SIS
(EL
EC
TIV
E – I)
UN
IT – I
ME
AS
UR
EM
EN
TS
Basic principles, A
ccuracy, Sensitivity, R
ange Measurem
ents, Errors.
UN
IT – II
EX
TE
NS
OM
ET
ER
S
Mechanical, O
ptical, Acoustical and E
lectrical extensometers and their use –
Advantage and disadvantage.
UN
IT – III
ST
RA
IN G
AU
GE
- PR
INC
IPL
ES
Principles and operation of electrical strain gauge- R
equirement - T
ype and theiruses, M
aterial for strain gauge, Calibration, C
ross sensitivity, Rosette A
nalysis.
UN
IT - IV
ST
RA
IN G
AU
GE
– ST
RA
IN M
EA
SU
RE
ME
NT
Wh
ea
tston
e b
ridg
e a
nd
po
ten
tiom
ete
r circuits fo
r static a
nd
dyn
am
ic strain
measurem
ents, Strain indicator.
UN
IT – V
PH
OT
OE
LA
ST
ICIT
Y
Tw
o dimensional P
hotoelasticity, Concept of Light – P
hoto–elastic effects, Stress
and optic law.
UN
IT – V
IF
RIN
GE
INT
ER
PO
LA
TIO
N T
EC
HN
IQU
SIn
terp
reta
tion
of frin
ge
pa
ttern
, Co
mp
en
satio
n a
nd
sep
ara
tion
tech
niq
ue
s,P
hotoelastic material.
UN
IT – V
IIN
ON
-DE
ST
RU
CT
IVE
TE
ST
ING
– I
Fu
nd
am
en
tals
of
No
n
De
structive
T
estin
g,
Ra
dio
gra
ph
y, U
ltraso
nic
Inspection,Ultrasonic C
-Scan, M
agnetic particles Inspection, Fluorescent penetrant
technique, Eddy current testing, A
coustic Em
ission Technique.
UN
IT – V
IIIN
ON
-DE
ST
RU
CT
IVE
TE
ST
ING
– II
Fu
nd
am
en
tals o
f brittle
coa
ting
me
tho
ds, In
tod
uctio
n to
Mo
iré T
ech
niq
ue
s,H
olography, Therm
ography.
TE
XT
BO
OK
S
1.D
aily, J.W., and R
iley, W.F
., Experim
ental Stress A
nalysis, McG
raw H
ill Inc.,N
ew Y
ork 19782.
Mechanical M
easurement / B
eckwith, M
aragoni and Lienhard / Addision –
Wesley
RE
FE
RE
NC
ES
1.H
etyenyi, M., H
and Book of E
xperimental S
tress Analysis, John W
iley andS
ons INC
., New
York, 1972
2.S
rina
th, L
.S., R
ag
ha
va, M
.R., L
ing
aia
h, K
., Ga
rge
sha
, G. P
an
t B., a
nd
Ram
achandra, K., E
xperimental S
tress Analysis, T
ata McG
raw H
ill, New
Delhi,
1984.3.
Pollock A
.A., A
coustic Em
ission in Acoustics and V
ibration Progress, S
tephensR
.W.B
., Chapm
an and Hall, 1983.
4.M
anufacturing Engineering T
echnology, Kalpakajam
/ Addision W
esley.
2005-20062005-2006
44
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
IV Y
ear B. T
ech. A
E – I sem
esterT
P C
4+1 0 4
(AE
05063) AV
ION
ICS
(Elective-1)
UN
IT –I
BA
SIC
S
Basic principles of A
vionics – Typical avionics sub system
in civil/ military aircraft
and space vehicles.
UN
IT –II
FL
IGH
T D
EC
K A
ND
DIS
PL
AY
SY
ST
EM
S
Flight deck display technologies – C
RT
, LED
, LCD
, Touch screen – H
ead up display– E
lectronic instrumentation system
s.
UN
IT-III
AU
DIO
AN
D C
OM
MU
NIC
AT
ION
SY
ST
EM
S
Aircraft audio system
s basic – audio transmitter and receiver principles – V
HF
comm
unication system – U
HF
comm
unication systems.
UN
IT-IV
RA
NG
ING
AN
D L
AN
DIN
G S
YS
TE
MS
VH
F O
mnirange – V
OR
receiver principles – distance maturity equipm
ent – principlesof operation – Instrum
ent landing system – localizer and glideslope.
UN
IT-V
PO
SIT
ION
G S
YS
TE
M
Global positioning system
principles – triangulation – position accuracy – applicationsin aviation.
UN
IT-V
IIN
ER
TIA
L N
AV
IGA
TIO
N S
YS
TE
M
Principle of O
peration of INS
– navigation over earth – components of inertial
Navigation system
s – accelerometers – gyros and stabilized platform
.
UN
IT-V
IIS
UR
VE
LL
IEN
CE
SY
ST
EM
AT
C surveillance system
s principles and operation interrogation and replay standards– C
ollision avoidance system – ground proxim
ity warning system
.
UN
IT-V
IIIA
UT
O F
LIG
HT
SY
ST
EM
Autom
atic flight control systems – fly by w
ire and fly by light technologies – flightdirector system
s – flight managem
ent systems. Integrated D
AT
AT
RA
NS
FE
Rm
ethodology by use of MILS
– ST
D – 1553/ A
RIN
C – 429.
TE
XT
BO
OK
S
1.E
lements of electronic navigation, N
.S.N
agaraja, Tata M
c Graw
Hill, 1995.
2.A
vionic systems O
peration and maintenance, Janes W
.Wasson, Jeppesen
Sandersen T
raining products (Sterling B
ook House, M
umbai),1994.
RE
FE
RE
NC
ES
1.P
rinciple of Avionics, A
lbert Hel frick, A
vionics Com
munications Inc., 2000.
2.A
ircraft Instrumentation and Integrated system
s EH
J Pallet, Longan S
cientificT
echnical (Sterling B
ook House, M
umbai) 1996.
3.A
ircraft Radio S
ystems, J.P
owell, P
itman publishers, 1998.
2005-20062005-2006
45
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DIV
Year B
. Tech
. AE
– I semester
T P
C4+1 0 4
(AE
05290) HE
LIC
OP
TE
R E
NG
INE
ER
ING
(Elective-1)
UN
IT - IE
LEM
EN
TS O
F HE
LICO
PTE
R A
ER
OD
YN
AM
ICS
Configurations based on torque reaction - Jet rotors and com
pound helicopters.U
NIT – II
RO
TOR
CO
NTR
OL
Methods of control - C
ollective and cyclic pitch changes - Lead-lag and flapping hinges.U
NIT - III
IDE
AL R
OTA
R TH
EO
RY
Hovering perform
ances - Mom
entum and sim
ple blade element theories.
UN
IT – IVR
OTO
R P
ER
FOR
MA
NC
EFigures of m
erit - Profile and induced pow
er estimation - C
onstant chord and ideal twist
rotors.U
NIT - V
PO
WE
R E
STIM
ATE
SInduced, P
rofile and Parasite pow
er requirements in forw
ard flight - Perform
ances curvesw
ith effects of altitude.U
NIT – V
IS
TAB
ILITY A
ND
TRIM
Prelim
inary ideas on helicopter stability.U
NIT - V
IILIFT A
ND
CO
NTR
OL O
F V/S
TOL A
IRC
RA
FTVarious configuration - P
ropeller, Rotor ducted fan and jet lift - Tilt w
ing and vectoredthrust - P
erformances of V
TOL and S
TOL aircraft in hover, Transition and Forw
ard motion.
UN
IT - VIII
GR
OU
ND
EFFE
CT M
AC
HIN
ES
Types - Hover height, Lift augm
entation and power calculations for plenum
chamber and
peripheral jet machines - D
rag of hovercraft on land and water. A
pplications of hovercraft.TE
XT B
OO
KS
1.Johnson, W
., Helicopter Theory, P
rinceton University P
res, 1980.2.
McC
ormick, B
.W., A
erodynamics, A
eronautics & Flight M
echanics John Wiley, 1995
RE
FER
EN
CE
S1.
Gessow
, A., and M
yers, G.C
., Aerodynam
ics of Helicopter, M
acmillan &
Co.,
N.Y.1987.
2.M
cCorm
ick, B.W
., Aerodynam
ics of V/S
TOL Flight, A
cademics P
ress, 19873.
Gupta, L H
elicopter Engineering, H
imalayan books, 1996.
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
IV Y
ear B. T
ech. A
E – I sem
esterT
P C
4+1 0 4
(AE
05225) EN
GIN
EE
RIN
G O
PT
IMIZ
AT
ION
(Elective-I)
UN
IT-I
INT
RO
DU
CT
ION
TO
OP
TIM
IZA
TIO
N
Statem
ent of an Optim
ization Problem
-Classification of O
ptimization P
roblems-Local
and Global O
ptima
UN
IT-II
CL
AS
SIC
AL
OP
TIM
IZA
TIO
N T
EC
HN
IQU
ES
Single V
ariable Optim
ization-Multivariable O
ptimization w
ith Equality C
onstraints-D
irect Substitution-M
ethod of Constrained V
ariation- Method of Lagrange M
ultipliers
UN
IT-III
LIN
EA
R P
RO
GR
AM
MIN
G
Applications of Linear P
rogramm
ing-Standard form
of a Linear Program
ming
Problem
-Solution by graphical m
ethod-Sim
plex Method; T
wo phase and B
ig Mm
ethods-Revised sim
plex method- D
uality in Linear Program
ming
UN
IT-IV
TR
AN
SP
OR
TA
TIO
N A
ND
AS
SIG
NM
EN
T P
RO
BL
EM
S
Transportation P
roblem- N
orth west corner m
ethod-Vogel’s approxim
ation method-
MO
D m
ethod-Assignm
ent problems
UN
IT-V
NO
N-L
INE
AR
PR
OG
RA
MM
ING
-UN
CO
NS
TR
AIN
ED
OP
TIM
IZA
TIO
NT
EC
HN
IQU
ES
Classification of U
nconstrained Minim
ization-Pow
ell’s M-S
teepest Dscent M
ethod-C
onjugate Gradient M
ethod-Marquardt M
ethod,Davidon-F
letcher-Pow
ell Method,
Broyden-F
letcher-Goldfarb-S
hanno Method
2005-20062005-2006
46
UN
IT-V
IN
ON
-LIN
EA
R P
RO
GR
AM
MIN
G -C
ON
ST
RA
INE
D O
PT
IMIZ
AT
ION
TE
CH
NIQ
UE
S
Characteristics of a C
onstrained Problem
-Rosen’s G
radient Projection M
ethod-P
enalty Function M
ethod
UN
IT-V
IIIN
TE
GE
R P
RO
GR
AM
MIN
G
Graphical R
epresentation-Cutting P
lane Method-B
ranch and Bound M
ethod
UN
IT-V
IIID
YN
AM
IC P
RO
GR
AM
MIN
G
Multi-stage decision process-C
omputational P
rocedures in dynamic program
ming
TE
XT
BO
OK
S
1.”E
ng
ine
erin
g O
ptim
izatio
n: T
he
ory a
nd
Pra
ctice”, S
.S.R
ao
, Ne
w A
ge
International(P) Ltd.
2.“O
ptim
izatio
n fo
r En
gin
ee
ring
Dsig
n:A
lgo
rithm
s an
d E
xam
ple
s”, K.D
eb
,P
rentice-Hall, N
ew D
elhi,1995.
RE
FE
RE
NC
ES
1.“Introduction to O
ptimum
design”, J.S.A
rora, McG
raw H
ill2.
“Num
erical Optim
ization Techniques for E
ngineering Design”, V
anderplatts,G
.N., M
cGraw
Hill
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DIV
Year B
. Tech
. AE
– I semester
T P
C4+1 0 4
(AE
05306) IND
US
TR
IAL
AE
RO
DY
NA
MIC
S(E
LE
CT
IVE
– I)
UN
IT-I - A
TM
OS
PH
ER
E
Types of w
inds, Causes of variation of w
ind, Effect of terrain on gradient height.
UN
IT-II - A
TM
OS
PH
ER
IC B
OU
ND
AR
Y L
AY
ER
Pressure and velocity distribution over the rising car, W
ind tunnel model for
atmospheric boundary layer, variation of drag force for various positions of the rising
car.
UN
IT –III - W
IND
EN
ER
GY
CO
LL
EC
TO
RS
-I
Horizontal axis and vertical axis m
achines, Pow
er coefficient, Betz coefficient by
mom
entum theory.
UN
IT –IV
- WIN
D E
NE
RG
Y C
OL
LE
CT
OR
S-II
Working principles of horizontal and vertical axis m
achines, Design of axial m
achines.
UN
IT –V
- VE
HIC
LE
AE
RO
DY
NA
MIC
S
Pow
er requirements and drag coefficients of autom
obiles, Effects of cut back angle,
Aerodynam
ics of trains and hovercraft.
UN
IT –V
I - BU
ILD
ING
AE
RO
DY
NA
MIC
S
Pressure distribution on low
-rise buildings, Wind forces on buildings, E
nvironmental
winds in city blocks, S
pecial problems of tall buildings, B
uilding codes, Building
ventilation and architectural aerodynamics, Interference effect of B
uilding.
UN
IT –V
II - FL
OW
IND
UC
ED
VIB
RA
TIO
NS
Effects of R
eynolds number on w
ake formation of bluff shapes, V
ortex inducedvibrations, G
alloping and stall flutter.
UN
IT-V
III - DE
SIG
N O
F C
HIM
NE
Y
Height of chim
ney for various gas effluents, Effective height of chim
ney, flume rise,
Different types of flum
e rise for various climatic conditions.
TE
XT
BO
OK
S
1.B
levins, R.D
., Flow
Induced Vibrations, V
an Nostard, 1990.
2.C
alvert, N.G
., Wind P
ower P
rinciples, Charles G
riffin & C
o., London, 1979.
RE
FE
RE
NC
ES
1.S
corer, R.S
., Environm
ental Aerodynam
ics, Ellis H
arwood Ltd, E
ngland, 1978
2.S
ovran, M., A
erodynamics D
rag Mechanism
s of Bluff B
odies and Road
Vehicles, P
lenum P
ress, N.Y
., 1978.
3.S
achs. P., W
ind Forces in E
ngineering, Pergam
on Press, 1988.
2005-20062005-2006
47
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
IV Y
ear B. T
ech. A
E – I S
emester
T P
C4+1 0 4
(AE
05003) AD
VA
NC
ED
CO
MP
UT
AT
ION
AL
FL
UID
DY
NA
MIC
S(E
LE
CT
IVE
– II )U
NIT
- IP
AN
EL
ME
TH
OD
S
Introduction to panel method, B
asic aspects of uniform source and vortex flow
s,S
ource panel method – N
on-lifting flows over arbitrary tw
o-dimensional bodies.
UN
IT – II
VO
RT
EX
PA
NE
L M
ET
HO
D
Vortex panel m
ethod – Lifting flows over arbitrary tw
o-dimensional bodies.
UN
IT – III
ME
TH
OD
OF
CH
AR
AC
TE
RIS
TIC
S
Introduction to numerical techniques for steady supersonic flow
s, Philosophy of
method of characteristics. D
etermination of characteristic lines – T
wo-dim
ensionalirrotational flow
. Determ
ination of the compatibility equation and unit processes.
Regions of influence and D
omains of dependence.
UN
IT – IV
AP
PL
ICA
TIO
NS
OF
ME
TH
OD
OF
CH
AR
AC
TE
RIS
TIC
S
Supersonic nozzle design using m
ethod of characteristics - Description of M
cC
ormack’s predictors - C
orrector techniques.
UN
IT - V
TR
AN
SO
NIC
RE
LA
XA
TIO
N M
ET
HO
D
Theoretical aspects of transonic flow
s, Sm
all Perturbation flow
s - Transonic sm
allperturbation equations - C
entral and Backw
ard difference schemes, S
hock capturingvs. shock fitting techniques: C
onservation vs. non conservation forms of governing
equations, Line relaxation techniques.
UN
IT - V
IB
OU
ND
AR
Y L
AY
ER
EQ
UA
TIO
N
Introduction to boundary layer equations and their solutions. Description of the
boundary layer equations. Transform
ation of boundary layer equations and thenum
erical solution method. C
hoice of discretization model and the generalized C
rank-
Nicholson S
cheme. D
iscretization of boundary layer equations and illustration ofsolutions of a tridiagonal system
of linear algebraic equations.U
NIT
- VII
TIM
E D
EP
EN
DE
NT
ME
TH
OD
S – I
Stability of S
olution, Explicit tim
e dependent methods - E
uler, Backw
ard Euler, O
nestep trapezoidal, B
ackward differencing, m
ethods, Leap Frog m
ethod.
UN
IT – V
IIIT
IME
DE
PE
ND
EN
T M
ET
HO
DS
– II
Description of Lax-W
endroff Schem
e and Mac C
ormack’s tw
o-step predictor –C
orrector method. D
escription of time split m
ethods and Approxim
ate factorizationschem
es
TE
XT
BO
OK
S
1.John .D
. Anderson “ C
omputational F
luid Dynam
ics”, McG
raw H
ill
2.A
nderson, Dale A
., John C. T
anhill and Richard H
.P Letcher, “C
omputational
Flu
id M
ech
an
ics an
d H
ea
t tran
sfer”, M
cGra
w H
ill, Ne
w Y
ork 1
98
4,
Volum
es I & II.
RE
FE
RE
NC
ES
1.H
offmann, K
.A: C
omputational F
luid Dynam
ics for Engineers, E
ngineering
Education S
ystem, A
ustin, Tex., 1989
2.K
reyszig, E., A
dvanced Engineering M
athematics, W
iley, New
York
3.Introduction to C
omputational F
luid Dynam
ics, Chow
CY
, John Wiley, 1979
4.B
ose, T.K
., Com
putation Fluid D
ynamics, W
iley Eastern Ltd., 1988.
5.C
how, C
.Y., Introduction to C
omputational F
luid Dynam
ics, John Wiley, 1979.
6.H
irsch, A.A
., Introduction to Com
putational Fluid dynam
ics, Mcgraw
Hill, 1989.
7.F
letcher, Com
putational Fluid D
ynamics, V
ol I & II, S
pringer Verlag, 1993.
8.P
atankar, S.V
., Num
erical heat Transfer and F
luid Flow
. Hem
ispher Publishing
Corporation, 1992.
2005-20062005-2006
48
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DIV
Year B
. Tech
. AE
– I Sem
esterT
P C
4+1 0 4(M
E05108) C
AD
/CA
M(E
LE
CT
IVE
– II)U
NIT
– IC
omputers in Industrial M
anufacturing, Product cycle, C
AD
/ CA
M H
ardware, B
asicstructure, C
PU
, Mem
ory types, input devices, display devices, hard copy devices,storage devices.U
NIT
– IIC
omputer G
raphics : Raster scan graphics coordinate system
, database structurefor graphics m
odeling, transformation of geom
etry, 3D transform
ations, mathem
aticsof projections, clipping, hidden surface rem
oval.U
NIT
– IIIG
eometric m
odeling : Requirem
ents, geometric m
odels, geometric construction
models, curve representation m
ethods, surface representation methods, m
odelingfacilities desired.U
NIT
– IVD
rafting and Modeling system
s : Basic geom
etric comm
ands, layers, display controlcom
mands, editing, dim
ensioning, solid modeling, constraint based m
odeling.U
NIT
– VN
umerical control : N
C, N
C m
odes, NC
elements, N
C m
achine tools, structure ofC
NC
machine tools, features of M
achining center, turning center, CN
C P
artP
rogramm
ing : fundamentals, m
anual part programm
ing methods, C
omputer A
idedP
art Program
ming.
UN
IT – V
IG
roup Tech : P
art family, coding and classification, production flow
analysis,advantages and lim
itations, Com
puter Aided P
rocesses Planning, R
etrieval typeand G
enerative type.U
NIT
– VII
Material requirem
ent planning, manufacturing resources planning, D
NC
, AG
V,
AS
RS
, Flexible m
anufacturing systems – F
MS
equipment, system
layouts, FM
Scontrol.U
NIT
– VIII
CIM
: Integration, CIM
implem
entation, major functions in C
IM, B
enefits of CIM
,Lean m
anufacturing, Just-in-time.
Text B
oo
ks :1.
CA
D / C
AM
Principles and A
pplications – 2nd edition, P
.N. R
ao, Tata M
c. Graw
Hill
RE
FE
RE
NC
ES
:1.
CA
D / C
AM
Theory and P
ractice / Ibrahim Z
eid / TM
H2.
CA
D / C
AM
/ CIM
/ Radhakrishnan and S
ubramanian / N
ew A
ge3.
Principles of C
omputer A
ided Design and M
anufacturing / Farid A
mirouche /
Pearson
4.C
omputer N
umerical C
ontrol Concepts and program
ming / W
arren S S
eames
/ Thom
son.5.
CA
D / C
AM
by CS
P R
ao – Hi-T
ech Publishers.
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
IV Y
ear B. T
ech. A
E – I S
emester
T P
C4+1* 0 4
(AE
05509) RO
CK
ET
S A
ND
MIS
SIL
ES
(EL
EC
TIV
E – II)
UN
IT-I
SO
LID
PR
OP
EL
LA
NT
RO
CK
ET
SY
ST
EM
S
Ignition system in rockets-T
ypes of igniters-Igniter design considerations- Com
bustionsystem
of solid rockets
UN
IT-II
LIQ
UID
PR
OP
EL
LA
NT
RO
CK
ET
SY
ST
EM
S
Design consideration of liquid rocket com
bustion chamber, injector, propellant feed
lines, valves, propellant tank outlet and helium pressurized and turbine feed system
s-P
ropellant slosh - Propellant ham
mer- G
eysering effect in cryogenic rocket engines
UN
IT-III
AE
RO
DY
NA
MIC
S O
F R
OC
KE
TS
AN
D M
ISS
ILE
S
Airfram
e components of rockets and m
issiles- Forces acting on a m
issile while
passing through atmosphere- C
lassification of missiles- M
ethod of describingaerodynam
ic forces and mom
ents-Lateral aerodynamic m
oment-Lateral dam
pingm
oment and longitudinal m
oment of a rocket-Lift and drag forces-D
rag estimation-
Body upw
ash and downw
ash in missiles-R
ocket dispersion.
UN
IT-IV
TW
O-D
IME
NS
ION
AL
RO
CK
ET
MO
TIO
N IN
VA
CU
UM
Equations of m
otion-Rocket M
otion in free space (Tsiokovsky’s equation, R
ocketP
ara
me
ters, B
urn
ou
t ran
ge
)-Ro
cket M
otio
n in
a h
om
og
en
eo
us g
ravita
tion
al
field(Vertical flight, C
onstant Pitch angle, G
ravity turns)
UN
IT-V
MU
LT
I-ST
AG
E R
OC
KE
T
Nom
enclature of the multi-stage rocket-Ideal V
elocity of the multi-stage rocket-V
erticalascent in a hom
ogeneous gravitational field and in vacuum (B
urnout velocity-C
ulmination altitude-V
ertical ascent of a two-stage rocket)
2005-20062005-2006
49
UN
IT-V
IA
TT
ITU
DE
CO
NT
RO
L O
F R
OC
KE
TS
AN
D M
ISS
ILE
S
Rocket thrust vector control - M
ethods of thrust vector control-Thrust m
agnitudecontrol, T
hrust Term
ination
UN
IT-V
IIS
EP
AR
AT
ION
SY
ST
EM
S F
OR
RO
CK
ET
S A
ND
MIS
SIL
ES
Stage separation dynam
ics-Separation techniques
UN
IT-V
IIIM
AT
ER
IAL
S F
OR
RO
CK
ET
S A
ND
MIS
SIL
ES
Criteria for S
election of materials for rockets and m
issiles-Choice of m
aterials atcryogenic tem
peratures, extremely high tem
peratures - Requirem
ent of materials
for thermal protection and pressure vessels
TE
XT
BO
OK
S
1.“R
ocket Propulsion E
lements”, G
eorge P. S
utton and Oscar B
iblarz, Wiley-
Interscience, 20002.
“Ro
cket P
rop
ulsio
n a
nd
Sp
ace
fligh
t Dyn
am
ics”, J.W. C
orn
elisse
,H
.F.R
.Schoyer, and K
.F.W
akker, Pitm
an, 1979
RE
FE
RE
NC
ES
1.“M
issile Configuration D
esign”, SS
Chin, M
cGraw
Hill, N
Y, 1961
2.”S
pace Vehicle D
ynamics”, K
.J.Ball and G
.F.O
sborne, Oxford U
niversityP
ress, 19673.
“Materials for M
issiles and Spacecraft”, E
.R. P
arker, McG
raw H
ill, 1982.
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
IV Y
ear B. T
ech. A
E – I S
emester
T P
C4+1 0 4
(AE
05496) PR
OP
EL
LA
NT
TE
CH
NO
LO
GY
(EL
EC
TIV
E – II)
UN
IT - I
LIQ
UID
FU
EL
S
Properties and tests for petroleum
products - Motor gasoline - A
viation gasoline -A
viation turbine fuels - Requirem
ents of aviation fuels of kerosene type and high
flash point type - Requirem
ents for fuel oils.
UN
IT - II
SO
LID
PR
OP
EL
LA
NT
S – I
Single base propellants - D
ouble base propellants - Com
posite propellants - CM
BD
propellants - Metallized com
posite propellants.
UN
IT - III
SO
LID
PR
OP
EL
LA
NT
S – II
Intro
du
ction
to d
iffere
nt fu
els a
nd
oxid
izers o
f com
po
site p
rop
ella
nts - B
rief
introduction to composite theory of com
posite and double base propellants.
UN
IT - IV
LIQ
UID
PR
OP
EL
LA
NT
S – I
Various liquid propellants and their properties - M
onopropellants and bipropellant
system - concept of ullage - Ignition studies of liquid propellants.
UN
IT - V
LIQ
UID
PR
OP
EL
LA
NT
S – II
Propellant loading tolerances - inventory - V
olume versus m
ass loading - Loadingm
easurement and control - O
utage control.
2005-20062005-2006
50
UN
IT –V
IC
RY
OG
EN
IC P
RO
PE
LL
AN
TS
– I
Introduction to cryogenic propellants - Liquid hydrogen, liquid oxygen, liquid nitrogenand liquid nitrogen and liquid helium
and their properties.
UN
IT –V
IIC
RY
OG
EN
IC P
RO
PE
LL
AN
TS
– IIT
heory behind the production of low tem
perature - Expansion engine - C
ascadeprocess - Joule T
hompson effect - M
agnetic effect - Ortho and para H
2 - Helium
4
and Helium
3 - Ideal cycles and efficiency of cryo systems - S
toring of cryogenic
propellants - Cryogenic loading problem
s.
UN
IT - V
IIIP
RO
PE
LL
AN
T T
ES
TIN
G
Laboratory testing - Arc Im
age Furnace - Ignitability studies - D
ifferential Therm
al
Analysis - T
hermo-gravim
etric analysis - Particle size m
easurement M
icro-merograph
- Strand burner tests im
pulse bomb - P
erformance estim
ation.
TE
XT
BO
OK
S
1.C
ornelissse, J.W., R
ocket Propulsion and S
pace Dynam
ics, J.W. F
reeman &
Co., Ltd., London, 1980.
2.P
anrner, S.F
. Propellant C
hemistry, R
einhold Publishing C
orp., N.Y
1985.
RE
FE
RE
NC
ES
1.S
hutton, G.P
., Rocket P
ropulsion Elem
ents, John Wiley, 1993.
2.S
harma, S
.P. and M
ohan .C., F
uels and Com
bustion, Tata M
cGraw
Hill
Publishing C
o, Ltd., 1984
3.M
athur, M., and S
harma, R
.P., G
as Turbine and Jet and R
ocket Propulsion,
Standard P
ublishers, New
Delhi, 1988.
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
IV Y
ear B. T
ech. A
E – I S
emester
T P
C4+1 0 4
(EE
05425) NE
UR
AL
NE
TW
OR
KS
& F
UZ
ZY
LO
GIC
(EL
EC
TIV
E – II)
UN
IT – I
INT
RO
DU
CT
ION
TO
NE
UR
AL
NE
TW
OR
KS
Introduction, Hum
ans and Com
puters, Organization of the B
rain, Biological N
euron,B
iological and Artificial N
euron Models, H
odgkin-Huxley N
euron Model, Integrate-
and-Fire N
euron Model, S
piking Neuron M
odel, Characteristics of A
NN
, McC
ulloch-P
itts Model, H
istorical Developm
ents, Potential A
pplications of AN
N.
UN
IT- II
ES
SE
NT
IAL
S O
F A
RT
IFIC
IAL
NE
UR
AL
NE
TW
OR
KS
Artificial N
euron Model, O
perations of Artificial N
euron, Types of N
euron Activation
Function, A
NN
Architectures, C
lassification Taxonom
y of AN
N – C
onnectivity, Neural
Dynam
ics (Activation and S
ynaptic), Learning Strategy (S
upervised, Unsupervised,
Reinforcem
ent), Learning Rules, T
ypes of Application
UN
IT–III
SIN
GL
E L
AY
ER
FE
ED
FO
RW
AR
D N
EU
RA
L N
ET
WO
RK
S
Introduction, Perceptron M
odels: Discrete, C
ontinuous and Multi-C
ategory, Training
Algorithm
s: Discrete and C
ontinuous Perceptron N
etworks, P
erceptron Convergence
theorem, Lim
itations of the Perceptron M
odel, Applications.
UN
IT- IV
MU
LT
ILA
YE
R F
EE
D F
OR
WA
RD
NE
UR
AL
NE
TW
OR
KS
Credit A
ssignment P
roblem, G
eneralized Delta R
ule, Derivation of B
ackpropagation(B
P) T
raining, Sum
mary of B
ackpropagation Algorithm
, Kolm
ogorov Theorem
,Learning D
ifficulties and Improvem
ents.
UN
IT V
AS
SO
CIA
TIV
E M
EM
OR
IES
Paradigm
s of Associative M
emory, P
attern Mathem
atics, Hebbian Learning, G
eneralC
oncepts of Associative M
emory (A
ssociative Matrix, A
ssociation Rules, H
amm
ingD
istance, The Linear A
ssociator, Matrix M
emories, C
ontent Addressable M
emory),
Bidirectional A
ssociative Mem
ory (BA
M) A
rchitecture, BA
M T
raining Algorithm
s:
2005-20062005-2006
51
Storage and R
ecall Algorithm
, BA
M E
nergy Function, P
roof of BA
M S
tability Theorem
Architecture of H
opfield Netw
ork: Discrete and C
ontinuous versions, Storage and
Recall A
lgorithm, S
tability Analysis, C
apacity of the Hopfield N
etwork
Su
mm
ary a
nd
Discu
ssion
of In
stan
ce/M
em
ory B
ase
d L
ea
rnin
g A
lgo
rithm
s,A
pplications.
UN
IT – V
IC
LA
SS
ICA
L &
FU
ZZ
Y S
ET
S
Introduction to classical sets - properties, Operations and relations; F
uzzy sets,M
embership, U
ncertainty, Operations, properties, fuzzy relations, cardinalities,
mem
bership functions.
UN
IT V
IIF
UZ
ZY
LO
GIC
SY
ST
EM
CO
MP
ON
EN
TS
Fuzzification, M
embership value assignm
ent, development of rule base and decision
making system
, Defuzzification to crisp sets, D
efuzzification methods.
UN
IT V
IIIA
PP
LIC
AT
ION
S
Neu
ral netw
ork ap
plicatio
ns: P
rocess identification, control, fault diagnosis andload forecasting.
Fu
zzy log
ic app
lication
s: Fuzzy logic control and F
uzzy classification.
TE
XT
BO
OK
:1.
Neural N
etworks, F
uzzy logic, Genetic algorithm
s: synthesis and applicationsby R
ajasekharan and Rai – P
HI P
ublication.2.
Introduction to Artificial N
eural System
s - Jacek M. Z
uarda, Jaico Publishing
House, 1997.
RE
FE
RE
NC
ES
:
1.N
eural and Fuzzy S
ystems: F
oundation, Architectures and A
pplications, - N.
Yadaiah and S
. Bapi R
aju, Pearson E
ducation2.
Neural N
etworks – Jam
es A F
reeman and D
avis Skapura, P
earson, 2002.3.
Neural N
etworks – S
imon H
ykins , Pearson E
ducation4.
Neural E
ngineering by C.E
liasmith and C
H.A
nderson, PH
I5.
Neural N
etworks and F
uzzy Logic System
by Bork K
osk, PH
I Publications.
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
IV Y
ear B. T
ech. A
E – I sem
esterT
P C
0 – 3 – 2
(AE
05253) FL
IGH
T V
EH
ICL
E D
ES
IGN
LA
B
1.O
bjectives Requirem
ents of the vehicle
2.C
onceptual Sketch and first estim
ate of weight
3.Initial S
izing
4.F
uselage and control surfaces
5.C
onfiguration layout.
6.P
erformance and stability E
stimate
7.Load estim
ates
2005-20062005-2006
52
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
IV Y
ear B. T
ech. A
E – I sem
esterT
P C
0 – 3 – 2
(AE05532) STR
UC
TUR
AL A
NA
LYSIS AN
D D
ETAILED
DESIG
N LA
B
Design and A
nalysis of the following A
ircraft Com
ponents:-
1.Landing G
ear
2.W
ings
3.F
uselage
4.P
ropeller Shaft
5.P
ropeller Blades
6.N
ose Cone
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
IV Y
ear B. T
ech. A
E – II sem
esterT
P C
4+1 0 4(A
E05030) A
IRC
RA
FT
SY
ST
EM
S A
ND
INS
TR
UM
EN
TS
UN
IT - I
HY
DR
AU
LIC
SY
ST
EM
S
Study of typical w
orkable system – C
omponents – H
ydraulic system controllers –
Modes of operation
UN
IT – II
PN
EU
MA
TIC
AN
D L
AN
DIN
G G
EA
R S
YS
TE
MS
Pneum
atic systems – A
dvantages – Working principles – T
ypical air pressure system– B
rake system – T
ypical pneumatic pow
er system – C
omponents – Landing gear
systems – C
lassification – Shock absorbers – R
etractive mechanism
.
UN
IT – III
AIR
PL
AN
E C
ON
TR
OL
SY
ST
EM
S
Conventional system
s – Pow
er assisted and fully powered flight controls – P
ower
actuated systems – E
ngine control systems – P
ush pull rod system, F
lexible pushfull rod system
– Com
ponents.
UN
IT – IV
MO
DE
RN
CO
NT
RO
L S
YS
TE
MS
Dig
ital fly b
y wire
system
s – A
uto
pilo
t system
active
con
trol te
chn
olo
gy,
Com
munication and N
avigation systems – Instrum
ent landing systems, V
OR
– CC
V,
Case studies.
UN
IT - V
EN
GIN
E S
YS
TE
MS
Fuel system
for piston and jet engines - Com
ponents of multi engines – Lubricating
systems for piston and jet engines.
UN
IT – V
IS
TA
RT
ING
AN
D IG
NIT
ION
SY
ST
EM
S
Starting and Ignition system
s – Typical exam
ples for piston and jet engines.
2005-20062005-2006
53
UN
IT - V
IIA
IR C
ON
DIT
ION
ING
AN
D P
RE
SS
UR
IZIN
G S
YS
TE
MS
Basic air cycle system
s – Vapor cycle system
s, Boost – strap air cycle system
–E
vaporative vapor cycle systems – E
vaporative air cycle systems – O
xygen systems
– Fire protection system
s, De-icing and anti-icing system
s.
UN
IT - V
IIIA
IRC
RA
FT
INS
TR
UM
EN
TS
Flight instrum
ents and Navigation instrum
ents – Accelerom
eters, Air speed indicators
– Mach m
eters – Altim
eters – Principles and operation – S
tudy of various types ofengine instrum
ents – Tachom
eters – Tem
perature gauges – Pressure gauges –
Operation and principles.
TE
XT
BO
OK
S
1.M
cKinley, J.L., and B
ent, R.D
., Aircraft M
aintenance & R
epair, McG
raw H
ill,1993. T
ransportation, Federal A
viation Adm
inistration The E
nglish Book S
tore, New
Delhi, 1995
2.G
eneral Handbooks of A
irframe and P
ower P
lant Mechanics, U
.S.D
ept. of
RE
FE
RE
NC
ES
1.M
cKinley, J.L.and B
ent, R.D
., Aircraft P
ower P
lants, McG
raw H
ill 1993.2.
Pallet, E
.H.J., A
ircraft Instruments &
Principles, P
itman &
Co 1993.
3.T
reager, S., G
as Turbine T
echnology, McG
raw H
ill 1997.
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
IVY
ear B. T
ech. A
E – II sem
esterT
P C
4+1 0 4
(AE
05540) SY
ST
EM
MO
DE
LIN
G A
ND
SIM
UL
AT
ION
(EL
EC
TIV
E – III)
UN
IT I
BA
SIC
CO
NC
EP
TS
Hierarchy T
ypes – Elem
ents of a system – system
description – Modeling definition
– Functions, classification.
UN
IT II
SIM
UL
AT
ION
Structure of S
imulation M
odels – Modeling approaches – S
ystem sim
ulation –
Definition – T
he Sim
ulation process – Advantages
UN
IT III
TE
CH
NIQ
UE
S F
OR
RA
ND
OM
NU
MB
ER
GE
NE
RA
TIO
N
Sim
ulation of random phenom
ena – Monte-C
arlo sampling – R
andom num
ber
generation – Mid square m
ethod – Mid product m
ethod – Multiplicative congruential
method – A
dditive congruential method,
UN
IT IV
RA
ND
OM
NE
SS
TE
ST
ING
Testing for random
ness – Chi-square m
ethod – Kolm
ogrov method – R
uns test –
Gasp test.
2005-20062005-2006
54
UN
IT V
DA
TA
PR
EP
AR
AT
ION
Correlation and regression analysis – C
urve fitting – Fitting of know
n distributions –
Uniform
, normal, exponential P
oisson, Weibull em
pirical distribution – Tim
e flow
mechanism
– Flow
diagram
UN
IT V
I
SIM
UL
AT
ION
OF
DIS
CR
ET
E S
YS
TE
M – I
Sim
ulation of an event occurrence using random num
ber table – Sim
ulation of
component failure using exponential and W
eibull models
Sim
ulation of single server and two server queue – S
imulation of an inventory system
.
UN
IT V
II
SIM
UL
AT
ION
OF
DIS
CR
ET
E S
YS
TE
M – II
Planning of sim
ulation experiments – T
actical planning – Run length determ
ination
– Validation of sim
ulation models – A
nalysis of simulation results
UN
IT V
III
SIM
UL
AT
ION
LA
NG
UA
GE
S
Introduction – Basic C
oncepts and Advantages of G
PS
S – C
ase Exam
ple – Basic
concepts and advantages of SIM
SC
RIP
T – C
ase example.
TE
XT
BO
OK
S
1“S
ystem S
imulation w
ith Digital C
omputers”, N
arasingh Deo, P
HI, 1979.
2“S
ystem S
imulation”, G
eoffrey Gordon, P
HI, 1995.
RE
FE
RE
NC
ES
1“D
iscrete Event S
ystem S
imulation”, Jerry B
anks, John S. C
arson and Baryl
nelson., PH
I, 1996.
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DIV
Year B
. Tech
. AE
– II semester
T P
C4+1 0 4
(AE
05156) CR
YO
GE
NIC
S(E
LE
CT
IVE
– III)
UN
IT – I - IN
TR
OD
UC
TIO
N
Historical background – Introduction to cryogenic problem
s.
UN
IT – II - C
RY
OG
EN
IC P
RO
PE
LL
AN
TS
Liquid hydrogen, Liquid helium, Liquid nitrogen and Liquid oxygen and their properties.
UN
IT – III - P
RO
DU
CT
ION
OF
LO
W T
EM
PE
RA
TU
RE
Th
eo
ry be
hin
d th
e p
rod
uctio
n o
f low
tem
pe
ratu
re –
Exp
an
sion
en
gin
e h
ea
texchangers – C
ascade process Joule Thom
son effect – Magnetic effect - O
rtho andpara H
2 – Helium
4 and Helium
3.
UN
IT – IV
- EF
FIC
IEN
CY
OF
CR
YO
GE
NIC
SY
ST
EM
S
Types of losses and efficiency of cycles – S
pecific amount of cooling – T
he fractionliquefied – C
ooling coefficient of performance – T
hermodynam
ic efficiency – The
energy balance method.
UN
IT –V
- CY
CL
ES
OF
CR
YO
GE
NIC
PL
AN
TS
– I
Classification of cryogenic cycles – T
he structure of cycles – Throttle expansion
cycles – Expander cycles – num
erical problems.
UN
IT –V
I - CY
CL
ES
OF
CR
YO
GE
NIC
PL
AN
TS
– II
Mixed throttle expansion and expander cycles – T
hermodynam
ic analysis – Num
ericalproblem
s.
UN
IT – V
II - CR
YO
GE
NIC
S IN
AE
RO
SP
AC
E A
PP
LIC
AT
ION
S
Cryogenic liquids in m
issile launching and space simulation of cryogenic liquids –
Effect of cryogenic liquids on properties of A
erospace materials.
UN
IT – V
III - CR
YO
GE
NIC
PR
OB
LE
MS
Cryogenic loading problem
s – Zero gravity problem
s associated with cryogenic
propellants – Phenom
enon of tank collapse – Elim
ination of geysering effect inm
issiles.
TE
XT
BO
OK
S
1.“C
ryogenic System
s”, Barron R
F, O
xford Univ., 1985
2.“P
ropellant Chem
istry”, Parner S
F, R
einhold Pub. C
orp., NY
, 1985
RE
FE
RE
NC
E
1.“C
ryogenic Fundam
entals”, Haseldom
G, A
cademic P
ress, 1971
2005-20062005-2006
55
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
IV Y
ear B. T
ech. A
E – II S
emester
T P
C4+1 0 4
(EE
05404) MIC
RO
PR
OC
ES
SO
RS
& M
ICR
OC
ON
TR
OL
LE
RS
(EL
EC
TIV
E – III)
UN
IT –I
An over view
of 8085, Architecture of 8086 M
icroprocessor. Special functions of
General purpose registers. 8086 flag register and function of 8086 F
lags.U
NIT
–IIA
ddressing modes of 8086. Instruction set of 8086. A
ssembler directives, sim
pleprogram
s.U
NIT
– IIIA
ssembly language program
s involving, Logical, Branch &
Call instructions, sorting,
string manipulation.
UN
IT – IV
Pin diagram
of 8086-Minim
um m
ode and maxim
um m
ode of operation. Tim
ingdiagram
. Need for D
MA
. DM
A data transfer M
ethod, using 8237.U
NIT
- V8255 P
PI – various m
odes of operation and interfacing to 8086. Interfacing Keyboard,
Displays, S
tepper Motor and actuators. D
/A and A
/D converter interfacing.
UN
IT –V
IIn
terru
pt stru
cture
of 8
08
6. V
ecto
r inte
rrup
t tab
le. In
terru
pt se
rvice ro
utin
es.
Introduction to DO
S and B
IOS
interrupts. 8259 PIC
Architecture and interfacing
UN
IT –V
IIS
erial data transfer schemes. A
synchronous and Synchronous data transfer schem
es.8251 U
SA
RT
architecture and interfacing. TT
L –to – RS
232c andU
NIT
– VIII
8051 Microcontroller A
rchitecture, Register set of 8051, M
odes of timer operation,
Serial port operation, Interrupt structure of 8051, M
emory and I/O
interfacing of 8051.T
EX
T B
OO
KS
:1.
A.K
.Ray and K
.M.B
hurchandi – Advanced m
icroprocessor & P
reripherals,TM
H2.
Kenneth J. A
yala – 8051 Microcontroller, (P
enram International).
RE
FE
RE
NC
ES
:-1.
Y.LIU
and G.A
. Gibson M
icro computer system
s: The 8086/8088 F
amily
architecture, programm
ing and design 2nd ed, P
HI.
2.A
vatar singh and Triebel – M
icroprocessors 8086/ 8088 ,PH
I3.
Alan R
,Miller- A
ssembly Language T
echniques for the IBM
PC
,BP
B (for D
OS
and BIO
S interrupts only)
4.R
ajkamal, M
icro Controllers - P
earson Education, 2005.
5.D
esign with P
IC M
icro Controllers – John B
. Peatm
an, 2005.6.
8051 Micro C
ontrollers – Dr. R
ajiv Kapadia.
7.K
enneth J Ayala – 8086 M
icro Processor (P
ennam International).
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DIV
Year B
.Tech
AE
II Sem
esterT
P C
4+1 0 4(A
E05299) H
YP
ER
SO
NIC
AE
RO
DY
NA
MIC
S(E
LE
CT
IVE
-III)
UN
IT-I - F
UN
DA
ME
NT
AL
S O
F H
YP
ER
SO
NIC
FL
OW
S
Importance/properties of hypersonic flow
-Basic equations boundary conditions for
inviscid flow, shock w
ave shapes, flow over a w
edge
UN
IT-II - H
YP
ER
SO
NIC
AP
PR
OX
IMA
TIO
NS
Prandtl-M
eyer flow- A
xi-symm
etric flow over a cone - F
low over a flat plate
UN
IT-III - H
YP
ER
SO
NIC
SM
AL
L D
IST
UR
BA
NC
E T
HE
OR
Y
Flow
over a wedge and a cone- B
last wave analogy,-N
ewtonian im
pact theory-B
usemann centrifugal correction -S
hock expansion method- T
angent cone andtangent w
edge methods
UN
IT-IV
- BA
SIC
AS
PE
CT
S O
F H
YP
ER
SO
NIC
VIS
CO
US
FL
OW
S
Introduction to viscous flow and pressure interactions over a flat plate- B
oundarylayers
UN
IT-V
- HY
PE
RS
ON
IC A
ER
OD
YN
AM
IC H
EA
TIN
G
Reference tem
perature method-E
ntropy layer effects on aerodynamic heating
UN
IT-V
I - HY
PE
RS
ON
IC V
ISC
OU
S IN
TE
RA
CT
ION
S
Strong and w
eak interactions-Shock w
ave/ boundary layer interactions
UN
IT-V
II - HY
PE
RS
ON
IC V
EH
ICL
E D
ES
IGN
Hypersonic propulsion and vehicle design
UN
IT-V
III - RA
RE
FIE
D G
AS
DY
NA
MIC
S
Rarefied flow
regimes-K
inetic theory of gases-Gas-surface interaction-
Aerodynam
ic forces in hypersonic free molecular flow
around simple geom
etries
TEX
T BO
OK
S
1.“H
ypersonic and High Tem
perature Gas D
ynamics”, A
nderson, J.D,M
cGraw
-Hill,
1989.
2.“H
ypersonic Aerotherm
odynamics”, B
ertin, J.J., AIA
A, 1994.
RE
FER
EN
CE
S
1.“Introduction to H
ypersonic flow”, C
herni C G
, Academ
ic Press,1961
2.“H
ypersonic Flow Theory”, H
ayes W D
and Problein R
F, Academ
ic Press 1959
3.“E
lements of H
ypersonic Aerodynam
ics”, Cox R
N and C
rabtree L P, London1965
2005-20062005-2006
56
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
IV Y
ear B.T
ech A
E II S
emester
T P
C4+1 0 4
(AE
05524) SP
AC
E M
EC
HA
NIC
S(E
LE
CT
IVE
-III)
UN
IT-I
BA
SIC
CO
NC
EP
TS
The solar system
-Reference fram
es and coordinate systems-T
he celestial sphere-T
he ecliptic-Motion of vernal equinox-S
idereal time-S
olar Tim
e-Standard T
ime-T
heearth’s atm
osphere
UN
IT-II
TH
E G
EN
ER
AL
N-B
OD
Y P
RO
BL
EM
The m
any body problem-Lagrange-Jacobi identity-T
he circular restricted three- bodyproblem
-Libration points-Relative M
otion in the N-body problem
UN
IT-III
TH
E T
WO
-BO
DY
PR
OB
LE
M
Equations of m
otion-General characteristics of m
otion for different orbits-Relations
between position and tim
e for different orbits-Expansions in elliptic m
otion-Orbital
Elem
ents-Relation betw
een orbital elements and position and velocity
UN
IT-IV
TH
E L
AU
NC
HIN
G O
F A
SA
TE
LL
ITE
Launch vehicle ascent trajectories-General aspects of satellite injection-D
ependenceof orbital param
eters on in-plane injection parameters-Launch vehicle perform
ances-O
rbit deviations due to injection errors
UN
IT-V
PE
RT
UR
BE
D S
AT
EL
LIT
E O
RB
ITS
Special and general perturbations- C
owell’s M
ethod-Encke’s m
ethod-Method of
variations of orbital elements-G
eneral perturbations approach
UN
IT-V
IIN
TE
RP
LA
NE
TA
RY
TR
AJE
CT
OR
IES
Tw
o-dimensional interplanetary trajectories-F
ast interplanetary trajectories-Three-
dimensional interplanetary trajectories-Launch of interplanetary spacecraft-T
rajectoryabout the target planet
UN
IT-V
IIB
AL
LIS
TIC
MIS
SIL
E T
RA
JEC
TO
RIE
S
The boost phase-T
he ballistic phase-Trajectory geom
etry-Optim
al flights-Tim
e offlight-R
e-entry phase-The position of the im
pact point-Influence coefficients.
UN
IT-V
IIIL
OW
-TH
RU
ST
TR
AJE
CT
OR
IES
Eq
ua
tion
s of M
otio
n-C
on
stan
t rad
ial th
rust a
ccele
ratio
n-C
on
stan
t tan
ge
ntia
lthrust(C
haracteristics of the motion, Linearization of the equations of m
otion-P
erformance analysis
TE
XT
BO
OK
S
1.”R
ocket Propulsion and S
paceflight Dynam
ics”, J.W.C
ornelisse, H.F
.R. S
choyer,and K
.F. W
akker, Pitm
an, 1979
2.”S
paceflight Dynam
ics”, William
E.W
iesel, McG
raw-H
ill, 1997
RE
FE
RE
NC
ES
1."S
pacecraft Mission D
esign”, Charles D
.Brow
n, AIA
A E
ducation Series,
Published by A
IAA
, 1998
2.“O
rbital Mechanics”, V
ladimir A
. Chobotov, A
IAA
Education S
eries, AIA
AE
ducation Series, P
ublished by AIA
A, 2002
3.”F
un
da
me
nta
ls of A
strod
yna
mics a
nd
Ap
plica
tion
s”, Da
vid.A
. Ve
llad
o,
Microcosm
and Kluw
er, 2001
2005-20062005-2006
57
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DIV
Year B
.Tech
AE
II Sem
esterT
P C
4+1 0 4(A
E05244) F
AT
IGU
E A
ND
FR
AC
TU
RE
ME
CH
AN
ICS
(EL
EC
TIV
E-IV
)
UN
IT - I - F
AT
IGU
E O
F S
TR
UC
TU
RE
SS
-N C
urve
s - En
du
ran
ce lim
it - Effe
ct of m
ea
n stre
ss - No
tche
s an
d stre
ssconcentrations - N
euber’s stress concentration factors - Plastic stress concentration
factor - Notched S
-N curves.
UN
IT - II - D
ES
IGN
OF
CO
MP
ON
EN
TS
Goodm
an, Gerber and S
oderberg relations and diagrams – M
odified Goodm
anD
iagram – D
esign of components subjected to axial, bending, torsion loads and
combination of them
.
UN
IT - III - S
TA
TIS
TIC
AL
AS
PE
CT
S O
F F
AT
IGU
E B
EH
AV
IOU
RLow
cycle and high cycle fatigue - Coffin - M
anson’s relation – Transition life - C
yclicstrain hardening and softening.
UN
IT – IV
- LO
AD
AS
PE
CT
SA
nalysis of load histories - Cycle counting techniques - C
umulative dam
age - Miner’s
theory - Other theories.
UN
IT - V
- PH
YS
ICA
L A
SP
EC
TS
OF
FA
TIG
UE
Phase in fatigue life - C
rack initiation - Crack grow
th - Final fracture - D
islocations -F
atigue fracture surfaces.
UN
IT - V
I - FR
AC
TU
RE
ME
CH
AN
ICS
Strength of cracked bodies - P
otential energy and surface energy - Griffith’s theory
- Irwin-O
rwin extension of G
riffith’s theory to ductile materials.
UN
IT – V
II - ST
RE
SS
AN
AL
YS
ISS
tress analysis of cracked bodies - Effect of thickness on fracture toughness - S
tressintensity factors for typical geom
etries.
UN
IT – V
III - FA
TIG
UE
DE
SIG
N A
ND
TE
ST
ING
Safe life and fail-safe design philosophies – Im
portance of fracture mechanics in
aerospace structure - Application to com
posite materials structures.
TE
XT
BO
OK
1.K
no
tt, J.F., F
un
da
me
nta
ls of F
ractu
re M
ech
an
ics, Bu
tter W
orth
& C
o.,
(Publishers) Ltd., London, 1983
RE
FE
RE
NC
ES
1.B
arrois, W., and R
ipley, E.L., F
atigue of Aircraft S
tructures, Pergam
on Pres.,
Oxford, 1983.
2.S
ih, C.G
., Mechanics of F
racture, Vol. I, S
ijthoff and Noordhoff International
Publishing C
o., Netherlands, 1989.
3.“M
echanical Engineering D
esign” by J E S
higley.
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
IV Y
ear B.T
ech A
E II S
emester
T P
C4+1 0 4
(AE
05102) BO
UN
DA
RY
LA
YE
R T
HE
OR
Y(E
LE
CT
IVE
-IV)
UN
IT – I
BA
SIC
LA
WS
Basic law
s of fluid flow – C
ontinuity, mom
entum and energy equations as applied to
system and control volum
e – Concept of flow
fields.
UN
IT – II
FU
ND
AM
EN
TA
LS
OF
BO
UN
DA
RY
LA
YE
R T
HE
OR
Y
Viscous fluid flow
– Boundary conditions – D
evelopment of boundary layer –
Estim
ation of boundary layer thickness – Displacem
ent thickness, mom
entum and
energy thickness for two-dim
ensional flows. G
eneral stress system in a deform
ablebody – G
eneral strain system.
UN
IT - III
NA
VIE
R S
TO
KE
S E
QU
AT
ION
Relation betw
een stress and strain system in a solid body (H
ooke’s Law) – R
elationbetw
een stress and strain rate system in liquids and gases (S
troke’s Law) – T
heN
avier - Strokes E
quation (N-S
) – General properties of N
avier - Stokes E
quation.
UN
IT- IV
EX
AC
T S
OL
UT
ION
OF
N-S
EQ
UA
TIO
N
Tw
o dimensional flow
through a straight channel, Hagen –P
oiseulle flow – S
uddenlyaccelerated plane w
all – Flow
near a rotating disk – Very slow
motion: P
arallel flowpast a sphere.
UN
IT - V
LA
MIN
AR
BO
UN
DA
RY
LA
YE
R
Analysis of flow
past a flat plate and a cylinder – Integral relation of Karm
an –Integral analysis of energy equation – Lam
inar boundary layer equations – Flow
separation – Blasius solution for flat–plate flow
– Boundary layer tem
perature profilesfor constant plate tem
perature.
2005-20062005-2006
58
UN
IT – V
IB
OU
ND
AR
Y L
AY
ER
ME
TH
OD
S
Falkner S
kan Wedge flow
s – Integral equation of Boundary layer – P
ohlhausenm
ethod – Therm
al boundary calculations – One param
eter and two param
eterintegral m
ethods.
UN
IT – V
IIIN
CO
MP
RE
SS
IBL
E T
UR
BU
LE
NT
ME
AN
FL
OW
Tw
o-dimensional turbulent boundary layer equations – Integral relations – E
ddy-viscosity theories – V
elocity profiles.
UN
IT – V
IIIC
OM
PR
ES
SIB
LE
– BO
UN
DA
RY
LA
YE
R F
LO
W
The law
of the wall – T
he law of the w
ake – Turbulent flow
in pipes and channels –T
urbulent boundary on a flat plate – Boundary layers w
ith pressure gradient.
TE
XT
BO
OK
S
1.“T
urbulent Flow
s in Engineering”, R
eynolds AJ, John W
iley & S
ons, 19802.
“Incompressible F
low”, P
anton RL, John W
iley & S
ons, 1984
RE
FE
RE
NC
ES
1.“B
oundary Layer Theory”, S
chlichting H, M
cGraw
Hill, N
ew Y
ork, 19792.
“Viscous fluid F
low”, W
hite FM
, McG
raw H
ill Co. Inc., N
Y, 1991, 2
nd Edition
3.“F
undamentals of A
erodynamics”, A
nderson JD, M
cGraw
Hill B
ook Co., Inc.,
NY
, 2001, 3rd E
dition.
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
D
IV Y
ear B.T
ech A
E II S
emester
T P
C4+1 0 4
(AE
05334) INT
RO
DU
CT
ION
TO
AV
IAT
ION
MA
NA
GE
ME
NT
(EL
EC
TIV
E-IV
)
UN
IT-I
INT
RO
DU
CT
ION
TO
AIR
TR
AN
SP
OR
TA
TIO
NA
ir transportation industry-Regulation and A
dministration of air transportation-
Introduction to air carriers and general aviation
UN
IT-II
INT
RO
DU
CT
ION
TO
GE
NE
RA
L A
VIA
TIO
N M
AN
AG
EM
EN
T
An introductory study on principles of m
anagement applied to general aviation,
airlines- Includes topics on planning, organizing, directing, controlling and marketing
relating to the aviation industry.
UN
IT-III
FU
ND
AM
EN
TA
LS
OF
AIR
TR
AF
FIC
CO
NT
RO
L
Introduction to airspace systems-E
n-route/Term
inal Environm
ent-Pilot/C
ontrolleractions and responsibilities
UN
IT-III
INT
RO
DU
CT
ION
TO
AIR
LIN
ES
MA
NA
GE
ME
NT
Aircraft selection- R
oute feasibility analysis- Com
puterized Reservation S
ystemand M
anagement S
ystems- T
raffic Flow
Analysis-A
ircraft personnel and Flight
systems
UN
IT-V
AV
IAT
ION
EC
ON
OM
ICS
Introduction to economic considerations in A
irport and Airline m
anagements-
Pa
ssen
ge
r an
d C
arg
o T
ran
spo
rt Eco
no
mie
s-Lo
ad
Sh
arin
g a
nd
Op
era
tion
al
Econom
ics
UN
IT-V
IIN
TR
OD
UC
TIO
N T
O A
IRP
OR
T M
AN
AG
EM
EN
T
Major functions of airport m
anagement including facilities and services, organization,
human resources, m
aintenance, planning and zoning, operations, revenues andexpenses, public relations, ecology, and safety.
2005-20062005-2006
59
UN
IT-V
IIA
VIA
TIO
N M
AR
KE
TIN
G
Function of m
arketing in airline and general aviation operations-Market research-
De
ma
nd
an
alysis-A
dve
rtising
an
d P
rom
otio
n- S
ale
s traffic- T
he
ory o
f price
determination
UN
IT-V
III
INT
RO
DU
CT
ION
TO
AV
IAT
ION
SA
FE
TY
Basic principles of aviation accident prevention in A
irlines-Flight deck m
anagement
objectives and procedures-Hum
an factors for flight and ground personnel
TE
XT
BO
OK
S
1.“E
ssentials of Aviation M
anagement”, R
odwell Julie, K
endall Hunt P
ublishing
Co, 2003
2.“A
irline Managem
ent”, Charles B
anfe, Prentice H
all, 1991
RE
FE
RE
NC
ES
1.”A
irport Planning and M
anagement”, A
lexander T. W
ells, McG
raw H
ill, 2000
2.“A
viation Maintenance M
anagement”, H
arry A. K
innison, McG
raw H
ill,2004
3.“A
ir Transportation: A
Managem
ent Perspective”, A
lexander T. W
ells, Jhon G.
Wensveen, T
homson B
rooks/Cole, 2003
4.“B
usiness and Corporate A
viation: On D
emand M
anagement”, John J S
heehan,
McG
raw H
ill, 2003
5. “T
he
Airlin
e B
usin
ess in
the
21
st cen
tury”, R
iga
s Do
ga
nis, R
ou
tled
ge
,
Taylor&
Francis B
ooks Ltd,2000
6.“F
iscal Aspects of A
viation Managem
ent”, Robert W
. Kaps, S
outhern Illinois
University P
ress, 2000.
7.“A
irline Marketing and M
anagement”, S
tephen Shaw
, Ashgate P
ublishing,2004
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DIV
Year B
.Tech
AE
II Sem
esterT
P C
4+1 0 4(M
E05283) H
EA
T T
RA
NS
FE
R(E
LE
CT
IVE
-IV)
UN
IT – I
Intro
du
ction
: Modes and m
echanisms of heat transfer – B
asic laws of heat transfer
–General discussion about applications of heat transfer.
Co
nd
uctio
n H
eat Tran
sfer:F
ourier rate equation – General heat conduction equation in C
artesian, Cylindrical
and Spherical coordinates.
UN
IT – II
Sim
plification and forms of the field equation – steady, unsteady and periodic heat
transfer – Initial and boundary conditions.O
ne D
imen
sion
al Stead
y State C
on
du
ction
Heat T
ransfer:
Hom
ogeneous slabs, hollow cylinders and spheres – overall heat transfer coefficient
– electrical analogy – Critical radius of insulation
On
e Dim
ensio
nal S
teady S
tate Co
nd
uctio
n H
eat Tran
sfer:V
ariable Therm
al conductivity – systems w
ith heat sources or Heat generation
Extended surface (fins) H
eat Transfer – Long F
in, Fin w
ith insulated tip and Short
Fin, A
pplication to error measurem
ent of Tem
perature
UN
IT III
On
e Dim
ensio
nal T
ransien
t Co
nd
uctio
n H
eat Tran
sfer:S
ystems w
ith negligible internal resistance – Significance of B
iot and Fourier N
umbers
- Chart solutions of transient conduction system
s- Concept of F
unctional Body
UN
IT – IV
Co
nvective H
eat Tran
sfer:C
lassification of systems based on causation of flow
, condition of flow, configuration
of flow and m
edium of flow
– Dim
ensional analysis as a tool for experimental
investigation – Buckingham
Π T
heorem and m
ethod, application for developingsem
i – empirical non- dim
ensional correlation for convection heat transfer –S
ignificance of non-dimensional num
bers – Concepts of C
ontinuity, Mom
entum and
Energy E
quations.F
orced
con
vection
: Extern
al Flo
ws:
Concepts about hydrodynam
ic and thermal boundary layer and use of em
piricalcorrelations for convective heat transfer -F
lat plates and Cylinders
Intern
al Flo
ws:
Concepts about H
ydrodynamic and T
hermal E
ntry Lengths – Division of internal
flow based on this –U
se of empirical relations for H
orizontal Pipe F
low and annulus
flow.
2005-20062005-2006
60
UN
IT – V
Free C
on
vection
: Developm
ent of Hydrodynam
ic and thermal boundary layer along
a vertical plate - Use of em
pirical relations for Vertical plates and pipes.
UN
IT V
IH
eat Tran
sfer with
Ph
ase Ch
ang
e:B
oilin
g: – P
ool boiling – Regim
es – Calculations on N
ucleate boiling, Critical H
eatflux and F
ilm boiling.
Co
nd
ensatio
n: F
ilm w
ise and drop wise condensation –N
usselt’s Theory of
Condensation on a vertical plate - F
ilm condensation on vertical and horizontal
cylinders using empirical correlations.
UN
IT V
IIH
eat Exch
ang
ers:C
lassification of heat exchangers – overall heat transfer Coefficient and fouling
factor – Concepts of LM
TD
and NT
U m
ethods - Problem
s using LMT
D and N
TU
methods.
UN
IT V
IIIR
adiatio
n H
eat Tran
sfer :E
mission characteristics and law
s of black-body radiation – Irradiation – total andm
onochromatic quantities – law
s of Planck, W
ien, Kirchoff, Lam
bert, Stefan and
Boltzm
ann– heat exchange between tw
o black bodies – concepts of shape factor –E
missivity – heat exchange betw
een grey bodies – radiation shields – electricalanalogy for radiation netw
orks.
Tab
les/Co
des: H
eat and Mass transfer data book / C
.P. K
othandaraman,
Subram
anian/ New
Age P
ub.
TE
XT
BO
OK
S :
1.H
eat Transfer – G
hoshdastidar – Oxford U
niversity Press – II E
dition2.
Heat T
ransfer – P.K
.Nag/ T
MH
RE
FE
RE
NC
ES
:1.
Fundam
entals of Engg. H
eat and Mass T
ransfer / R.C
.SA
CH
DE
VA
/ New
Age
International2.
Essential H
eat Transfer - C
hristopher A Long / P
earson Education
3.H
eat Transfer – A
Practical A
pproach – Yunus C
engel, Boles / T
MH
4.H
eat and Mass T
ransfer – D.S
.Kum
ar / S.K
.Kataria &
Sons
5.H
eat Transfer / H
OLM
AN
/TM
H6.
Fundam
entals of Heat T
ransfer & M
ass Transfer- Incropera &
Dew
itt / JohnW
iley Pub.
7.E
ngineering Heat and M
ass Transfer – S
arit K. D
as / Dhanpat R
ai Pub.
8.H
eat and Mass T
ransfer – R. Y
adav /CP
H
JAW
AH
AR
LA
L N
EH
RU
TE
CH
NO
LO
GIC
AL
UN
IVE
RS
ITY
HY
DE
RA
BA
DIV
Year B
.Tech
AE
II Sem
esterT
P C
4+1 0 4(A
E05019) A
ER
OE
LA
ST
ICIT
Y(E
LE
CT
IVE
-IV)
UN
IT - I - A
ER
OE
LA
ST
ICIT
Y P
HE
NO
ME
NA
Sta
bility ve
rsus re
spo
nse
pro
ble
ms –
Th
e a
ero
-ela
stic trian
gle
of fo
rces -
Aeroelasticity in A
ircraft design – Prevention of A
eroelastic instability.
UN
IT – II - D
IVE
RG
EN
CE
OF
LIF
TIN
G S
UR
FA
CE
Sim
ple two-dim
ensional idealization – Strip theory – F
redholm integral equation of
the second kind –Exact solutions for sim
ple rectangular wings
UN
IT – III - A
PP
RO
XIM
AT
E S
OL
UT
ION
SS
emigrid assum
ptions and approximate solutions – G
eneralized coordinates –S
uccessive approximations –N
umerical approxim
ations using matrix equations.
UN
IT - IV
- ST
EA
DY
ST
AT
E A
ER
OE
LA
ST
IC P
RO
BL
EM
Loss and reversal of aileron control – Critical aileron reversal speed – A
ileronefficiency – S
emigrid theory and successive approxim
ations – Lift distribution –R
igid and elastic wings
UN
IT - V
- FL
UT
TE
R P
HE
NO
ME
NO
NN
on-dimensional P
arameters – S
tiffness criteria – Dynam
ic mass balancing – M
odelexperim
ents – Dim
ensional similarity – F
lutter analysis
UN
IT – V
I - QU
AS
I-ST
EA
DY
AN
AL
YS
IST
wo
dim
en
sion
al th
in a
irfoils in
stea
dy in
com
pre
ssible
flow
– Q
ua
si-stea
dy
aerodynamic derivatives – G
alerkin method for critical speed
UN
IT – V
II - DIS
TR
IBU
TE
D M
OT
ION
Stability of distributed m
otion –Torsion flexure flutter – S
olution of the flutterdeterm
inant – Methods of determ
ining the critical flutter speeds – Flutter prevention
and control.
UN
IT - V
III - EX
AM
PL
ES
OF
AE
RO
EL
AS
TIC
PR
OB
LE
MS
Galloping of transm
ission lines and flow induced vibrations of tall slender structures
and suspension bridges.
TEX
T BO
OK
S1.
Fung, Y.C., A
n introduction to the theory of Aeroelasticity, John W
iley and Sons
Inc., New
York, 1985.
2. S
canlan, R.H
. and Rosenbaum
, R., Introduction to the S
tudy of Aircraft V
ibrationand Flutter, M
cGraw
Co., N
.Y., 1991
RE
FER
EN
CE
S1.
Bisplinghoff, R
.L., Ashley, H
., and Halfm
ann, R.L., A
eroelasticity, Addison W
esleyP
ublishing Co., Inc., II ed, 1987
2.B
roadbent, E.G
., Elem
entary theory of Aeroelasticity, B
unHill P
ublication Ltd., 1986