bending stress.pptx
TRANSCRIPT
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JJ310- STRENGTH OF MATERIALS
BENDING STRESSES
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BENDING STRESS
1. To know about convention symbols for
bending stress
2. Derive the equation of bending
stresses
3. Understanding types of section
standard
4. Calculate the neutral axis (NA) for standard of
section
5. Calculate the second moment of
area (I) for the standard section
6. Use the bending equations to solve problems involving
strength and bending for the
simply supported and cantilever beam
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1. CONVENTION SYMBOLSSYMBOLS DESCRIPTION UNIT
E
F
I
Ic
IG
IPN
Ixx
M
R
Young’s Modulus
Concentrated Load
Second Moment Area
Second Moment Area around centroid axis
Second moment area around the center of gravity
Second moment area around the neutral axis
Second moment area around x – x axis
Bending Moment
Radius of Curvature
(
N/
m2
)
( N )
( m4 )
( m4 )
( m4 )
( m4 )
( m4 )
( Nm )
( m )
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STRESSES IN BEAMS
Forces and couples acting on the beam cause bending (flexural stresses) and shearing stresses on any cross section of the beam and deflection perpendicular to the longitudinal axis of the beam.
If couples are applied to the ends of the beam and no forces act on it, the bending is said to be pure bending. If forces produce the bending, the bending is called ordinary bending.
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ASSUMPTIONS
In using the following formulas for flexural and shearing stresses, it is assumed that:-
a plane section of the beam normal to its longitudinal axis prior to loading remains plane after the forces and couples have been applied
the beam is initially straight and of uniform cross section and that the modulus of elasticity in tension and compression are equal.
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ALLOCATION OF BENDING STRESS
y
M
M
P.N.
R
O
A’
B’E’
P’F’
Q’C’
D’
E
C D
QP
F
BA
MM
y
Rajah 9.2 (a)
Rajah 9.2 (b)
Referring on beside figure, the original position of the beam is shown partially in Figure 9.2 (a)
When the beam is curved, the part will be show as in Figure 9.2 (b).
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For such a curvature, the longitudinal layer of the beam along the top surface (AB) will be in compression, while the lower surface (CD) will be in tension.
Between the layers AB and CD, the length of one layer does not change when the bent beam.
y
M
M
P.N.
R
O
A’
B’E’
P’F’
Q’C’
D’
E
C D
QP
F
BA
MM
y
Rajah 9.2 (a)
Rajah 9.2 (b)
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The layers is called the neutral axis (N.A) or neutral plane.
The bending stress () at N.A = 0.
y
M
M
P.N.
R
O
A’
B’E’
P’F’
Q’C’
D’
E
C D
QP
F
BA
MM
y
Rajah 9.2 (a)
Rajah 9.2 (b)
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Distance of neutral axis from the center of curvature is called the radius of curvature (R).
For any layer of PQ (a distance y from the N.A) is curved and elongated and it become to P'Q'.
The layers along N.A become to E'F.
EF = E’F’ = R original length, PQ = EF = R
Final length, P’Q’ = (R+y)
y
M
M
P.N.
R
O
A’
B’E’
P’F’
Q’C’
D’
E
C D
QP
F
BA
MM
y
Rajah 9.2 (a)
Rajah 9.2 (b)
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length Original
PQ of elongation The Strain PQ
R
R - y) (R
R
y
R
y E PQ,at Stress
R
E
y
.......................eq. (1)
y
M
M
P.N.
R
O
A’
B’E’
P’F’
Q’C’
D’
E
C D
QP
F
BA
MM
y
Rajah 9.2 (a)
Rajah 9.2 (b)
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Rajah 9.2: Allocation of bending stress
N
AP
y
Based on Figure 9.2 (c), the cross section area for shaded strip is = A.
Suppose that the longitudinal stress on the line = .
The total moments of beam cross section:-
yA x y.R
E N.A aroundMoment
R
yE. σ proven,been Have
A.yR
E strip on the force theSo,
A.yR
E 2
A .yR
E M 2 I
R
E M
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Note;
But to balance the bending beam, the moment of resistance must be equal to the applied moments.
Therefore:-
When combined with equation 1, then:-
axis neutral around area secondmoment isA . I 2 y
R
E
I
M or I.
R
E M
R
E
y
σ
I
M This equation is used to solve
the problem of the bending stresses
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BENDING MOMENT OF BEAM (WITH UNIFORMLY DISTRIBUTED LOAD)
For Simply Supported Beam:-
8 wLM
2
max
The maximum bending moment can be determined using the formula below:
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For Cantilever Beam
2 wLM
2
max
The maximum bending moment can be determined using the formula below:
BENDING MOMENT OF BEAM (WITH UNIFORMLY DISTRIBUTED LOAD)
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WE WILL CONTINUE……….AFTER TAKE 5….
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EXERCISE:-
1. What is the meaning of symbol (I) in the general bending stress below
A. Second moment of inertiaB. CentroidC. Radius of curvatureD. Bending moment
R
E
y
σ
I
M
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EXERCISE:-
2. What is the meaning of symbol (M) in the general bending stress below
A. Second moment of inertiaB. CentroidC. Radius of curvatureD. Bending moment
R
E
y
σ
I
M
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EXERCISE:-
3. What is the meaning of symbol (y) in the general bending stress below
A. Second moment of inertiaB. CentroidC. Radius of curvatureD. Bending moment
R
E
y
σ
I
M
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EXERCISE:-
4.The formula bending moment for For Simply Supported Beam is:-
A.
B.
C.
2 wLM
2
max
8 wLM
2
max
16 wLM
2
max
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EXERCISE:-
5.The formula bending moment Cantilever Beam:-
A.
B.
C.
2 wLM
2
max
8 wLM
2
max
16 wLM
2
max
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ANSWER:-
1. A2. D3. B4. B5. A
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INTRODUCTION – SECOND MOMENT OF AREA
In this unit, the bending equation will be used to determine the bending stress of standard forms.
To obtain the bending stress, the position of neutral axis (N.A) and second moment of area (or moment of inertia) for standard forms (I) should be calculated.
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Rectangular: Second moment of area is defined as
Thus, for a rectangular section, second moment of area in PN, is
SECOND MOMENT OF AREA– RECTANGULAR SECTION
b
A B
dA
dy
y
DC
P.N.d
dA y I 2
12
bd
3
y b
dy y b
dy y I
3
2/
2/
3
2d/2
d/2-
22/
2/P.N.
d
d
d
d
Figure 10.1: Rectangular cross-section beam
Second moment of area at the N.A axis
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A
B
b bC
Dd
FE
P.N.
Rajah 10.2: Rasuk Berkeratan Rentas I
IN.A = IACEF – Ib.b ;
b.b = part of shaded area
12
)(bd 2 -
12
BD
33
To obtain the second
moment of area by using the cut-off
SECOND MOMENT OF AREA– RECTANGULAR I-SECTION
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Figure 10.3 shows a circle of radius r. The shaded elements shown in the figure has an area dA and therefore the following equation is formed: -
dA = rd
SECOND MOMENT OF AREA– CIRCULAR SECTION
dro
r
dr
Rajah 10.3: Rasuk Berkeratan Rentas Bulat
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From the polar coordinate system:-y = r sin
Second moment of area at N.A for a circular section is given by:-
SECOND MOMENT OF AREA– CIRCULAR SECTION
4
πr
θdθ sin 4
r
4
r dθ sinθ
θdr rd θ sin r
dA y I
4
22π
0
40
r
0
42π
0
22r
0
2π
0
2P.N.
0
o
dro
rdr
Rajah 10.3: The Circular cross section
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Parallel axis theorem states that the second moment of area on any axis parallel to the NA (the axis X - X) is equal to the second moment of area around the axis through the centroid of the (NA) plus the product of cross-sectional area and square of the distance between the axis parallel to the PN
THEOREM OF PARALLEL AXIS
P
y
N
h
dA
xx
y’
dA y I 2xx
Rajah 10.4: Rectangular section beam
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P
y
N
h
dA
xx
y’
Rajah 10.4: Rectangular section beam
If the NA line is drawn parallel to the line x-x, then the formula above can be described as follows: -
dAh dA y'2h dA )(y'
dAh h 2y' ) (y'
)h y' ( I
h y' y
22
22
2xx
THEOREM OF PARALLEL AXIS
The first integral is the second moment of area about an axis through the center of the form.
The second integral is the first moment of area about an axis through the center of the form, so it is equal to zero.
The last integral is to the total cross-sectional area. Next the equation above can be written as:-
dAy'
Ixx = IP.N. + Ah2NOTE: h = distance from the midpoint of
part of section in parallel with the neural axis.
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STANDARD SECTION SCHEDULE
From the equation that has been made, we can be brief as the table below: -
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STANDARD SECTION SCHEDULE
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CENTROID - A COMBINATION FORM
The form of a diagram can be produced by combining several basic form or cut the original diagram.
The form in Figure 10.5 (a) is produced by combining the rectangular ABCD with semicircular ADP.
D
CB
A
P
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CB
D
CB
DA A
P
C
p
D
y2
y1
A D
For Figure 10.5 (a) a high centroid of every basic form of BC is not the same that y1 y2
CENTROID - A COMBINATION FORM
y
Therefore,
Rajah 10.5(b)
)A (A
)yA y(A
A
Ay y
2 1
2211
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CENTROID - TRUNCATED FORM
In Figure 10.6 (a) part of square DEFG is cut and removed from the original rectangular form of ABCH.
CB
D
H
G
A
E
F
Rajah 10.6(a)
Figure 10.6 (a) a high centroid for each basic shape of the line BC is equal (Figure 10.6 (b)). So: -
y
CB
D
H
G
A
E
F
y2y1 D
G
E
F
CB
HA
Rajah 10.6(b)
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Referring to Figure 10.7, form of L can be produced by combining two rectangular or separated and cut methods of rectangular EDGF from ABCG.
y
y2
y1
E D
CB
FA
D
G
E
F
CB
GA
If using the cut and split, use the following formula:
)A (A
)yA y(A
A
Ay y
2 1
2211
CENTROID - TRUNCATED FORM
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If the for every layer of the upper surface to the bottom surface of the beam is determined, the values can be plotted on a graph as follows. The graph shows the distribution of the bending stress.
Look at the value of is not dependent on cross-sectional width of a strip. In layer N.A, = 0.
THE STRESS DISTRIBUTION
P.N.
5 cm
7 cm
- tensile
= 0
- compressive
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THANK YOU…
Q & A
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EXERCISE:-
1. The equation of the second moment of area for rectangular shape is:-
A.
B.
C.
D.
4
d2
12
d3
12
d4
4
d3
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2. The equation of the second moment of area for circular section is:-A.
B.
C.
D.
EXERCISE:-
4
r4
8
r4
4
r2
12
r2
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3. This below formula is state of :-
A. Second moment of area
B. Position of neutral axis
C. Theorem of parallel axis
D. Modulus of section
dA y I 2xx
EXERCISE:-
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4. Which is the formula is to determine the distance of centroid?A.
B.
C.
D.
EXERCISE:-
A
Ay
A
Ah
A
Ay 2
Ah
Ay
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5. Which if the unit of second moment of area?A. m4
B. m2
C. Nm2
D. N/m2
EXERCISE:-
6. Based the figure on right side, the label of x and y to determine second moment of area for rectangular shape is:- A. X = h and Y = dB. X = d and Y = bC. X = b and Y = dD. X = d and Y = h
X
Y
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EXERCISE:-
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EXAMPLE 1
A T bar with a length 6 meters incur of a concentrated load. Each load is 16 kN at a
distance of 1 m from both ends of the beam. Bar is simply supported on both ends as in
Figure 10.3 (a). The cross section bar is shown in Figure 10.3 (b). Calculate the following:
-
a. Distance of neutral axis from the bottom of the beam.
b. Second moment of area around the neutral axis.
c. The radius of curvature at the midspan of the beam.
d. Maximum the compressive and the tensile bending stress in the beam
Given E= 200 GN / m2
80 mm
20 mm
15 mm
60 mm
16 kN 16 kN
1 m1 m
6 m
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SOLUTION EXAMPLE 1:-
i. Calculate the distance of neutral axis from the bottom of the beam.
Step 1:
Divide of those sections into two parts. Calculate the centroid of the area and distance for each part of the sectional base.
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SOLUTION EXAMPLE 1:-
Step 2:
Determine the distance on the bottom of neutral axis cross section
mm 65
1200) 1200(
) 40 x (1200 ) 90 x (1200
AA
yA yA y
21
2211
Since we using the
method of cut sections, use this formula.
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Second moment of area at the neutral axis is
IP.N. = ( IC1 + A1h12 ) + ( IC2 + A2h2
2 )
= ( 40,000 + ( 1200 x 252 ) ) + ( 640,000 + ( 1200 x 252 ) )
= 2.18 x 106 mm4
= 2.18 x 10-6 m4
SOLUTION EXAMPLE 1:-ii. Calculate the second moment of area around the neutral axis.
Step 3:
Calculate the second moment of area and distance h for each section.
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iii. The radius of curvature at the midspan of the beam.
Step 4:
Use formula:-
From the loading shown, we find that the order of loading is symmetrical, so the reactions:-
R1 = R2 = 16 kN
From B.M.D, the bending moment of the midspan beam is:-
SOLUTION EXAMPLE 1:-
16 kN16 kN
1 m1 m
6 m
R1 R2
( + )
(-)
G.D.R
( + )
G.M.L.
M
EI R
R
E
y
I
M
M = 16 kNm ( hogging )
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SOLUTION EXAMPLE 1:-
m 27.25
10 x 16
10 x 2.18 x 10 x 200 R
3
-69
The radius of curvature at the midspan of the beam.
M
EI R
R
E
y
I
M
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SOLUTION EXAMPLE 1:-
iv. Maximum the compressive and the tensile bending stress in the
beam.
Step 5:
Refer to the diagram of the beam section, we find that:-
ylower > yupper
The maximum produced at the lower surface is :
ymax = 65 mm = 0.065 m
) tensile( N/mm 10 x 477
10 x 18.2
0.065 x 10 x 16
I
yM σ
26
6-
3maxmax
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The maximum produced at the upper surface is ,
ymax = 35 mm = 0.035 m
SOLUTION EXAMPLE 1:-
) ecompressiv ( N/m 10 x 256.8
10 x 18.2
0.035 x 10 x 16
I
yM σ
26
6-
3maxmax
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A 1 meter cantilever beam loads uniformly distributed along the span of the beam. Beam cross section is shown in below figure, where EE is the upper surface of the beam. Determine the the following: -
i. the neutral axis of cross section.
ii. Second moment of area around the neutral axis.
iii. Maximum tensile and compressive stress in the beam results from sagging.
80 mm
40 mm
60 mm
120 mm
E E
1 m
20 kN/m
EXAMPLE 2:
y
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Step 1:
Divide of those sections into two parts. Get wide and centroid of distance each part of the sectional base.
SOLUTION EXAMPLE 2:
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i. Distance of neutral axis on the bottom of the cross section.
SOLUTION EXAMPLE 2:
mm 70
4800) 4800(
) 40 x 4800 ( ) 100 x (4800
A A
21
2211
AA
yyy
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ii. Second moment of area around the neutral axis.
SOLUTION EXAMPLE 2:
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Second moment of area around the neutral axis.
IP.N. = ( IC1 + A1h12 ) + ( IC2 + A2h2
2 )
= ( 640 x 103 + ( 4800 x 302 ) ) + ( 2560 x 103 + ( 4800 x 302 ) )
= 11.84 x 106 mm4
= 1.184 x 10-5 m4
SOLUTION EXAMPLE 2:
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iii. Maximum bending moment occurs at the bar met the wall of :
Mmax = w L2 = (20 x 103) (12 ) = 10,000 Nm = 10 kNm
2 2
Since the beam is hogging, the top surface will have the lower surface tension and compression
SOLUTION EXAMPLE 2:
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ylower maximum = 70 mm
yupper maximum = 120 – 70 = 50 mm
SOLUTION EXAMPLE 2:
MN/m 59.12 10 x 1.184
10 x 70 x 10,000 ecompressiv σ
MN/m 42.23 10 x 1.184
10 x 50 x 10,000 tensileσ
I
yM σ
y
σ
I
M
25-
3-
max
25-
3-
max
maxmaxmax
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EXAMPLE 3:a. A cross section of a beam as shown in below figure.
Calculate :-i. The neutral axis for the beamii. second moment of area around the neutral axis.
b. If the beam is simply supported at both ends carrying a uniform load of 30 kN / m on the entire spans with a length 3m, calculate the bending stresses in the beam on: -
iii. the upper surfaceiv. the lower surface
80 mm
20 mm
20 mm10 mm
100 mm
10 mm
100 mm
P.N.
40 mm
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a. The section can be considered a T-shaped grafting yield from second and first part. While the center is divided punched a hole as rectangular shape (part 3).
Get area for each of divisions involved :-
Part 1 A1 = 80 x 20 = 1600 mm2
Part 2 A2 = 40 x 100 = 4000 mm2
Part 3 A3 = 20 x 100 = 2000 mm2
Calculate the distance y from the base of the T section.
y1 = 100 + 10 = 110 mm ; y2 = 50 mm;
y3 = 10 + 50 = 60 mm
SOLUTION EXAMPLE 3:
P.N.
1
2
3
80 mm20 mm
20 mm
10 mm
100 mm
10 mm
100 mm
P.N.
40 mm
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i. Dapatkan nilai
SOLUTION EXAMPLE 3:
P.N.
1
2
3
A
Ay y formulan menggunakadengan y
mm 71.1
2000) - 4000 1600(
60) x (2000 - 50) x (4000 110) x (1600
A A A
y A - y A y A y
321
332211
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ii. Get a second moment of area around the neutral axis.
h1 = y1 - = 110 – 65.3 = 44.7 mm
h2 = - y2 = 65.3 – 50 = 15.3 mm
h3 = - y3 = 65.3 – 60 = 5.3 mm
Get Ah2 value of each part.
A1h12 = 1600 x ( 44.7 )2 = 3.2 x 106 mm4
A2h22 = 4000 x ( 15.3 )2 = 936 x 103 mm4
A3h32 = 2000 x ( 5.30 )2 = 56 x 103 mm4
SOLUTION EXAMPLE 3:
_
y _
y _
y
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Use Ic = formula to determine second moment of
area for each section.
IC1 =
IC2 =
IC3 =
IP.N. = ( IC1 + A1h12 ) + ( IC2 + A2h2
2 ) - ( IC3 + A3h32 )
= 5.8 x 106 mm4
= 5.8 x 10-6 m4
SOLUTION EXAMPLE 3:
12
bd3
433
mm 10 x 53 12
20 x 80
433
mm 10 x 3.33 12
100 x 40
463
mm 10 x 1.67 12
100 x 20
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b. Get the reaction force at both ends A and B.
Total force on A = Total force on B RA = RB
Therefore, RA = RB =
Mmax will occur on midspan of the beam. Therefore,
Mmax = wL2 / 8
= 30 kN/m (32) / 8 = 33.75 kNm
SOLUTION EXAMPLE 3:
3 m
30 kN/m
RA RB
kN 45kN 2
330
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SOLUTION EXAMPLE 3:
I
y M σ
y
σ
I
M maxmaxmax
26-
3
upper MN/m 318 x108.5
0.0547 x 10 x 33.75 σ
26-
3
lower MN/m 380 x108.5
0.0653 x 10 x 33.75 σ
We obtained that :
ylower = 65.3 mm Therefore, yupper = 120 – 65.3 = 54.7 mm
Thus;
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EXERCISE A 5 m cantilever beam loads uniformly distributed along
the span of the beam. Beam cross section is shown in the figure below, where EE is the upper surface of the beam. Determine the the following: -
i. the neutral axis of cross section.
ii. Second moment of area around the neutral axis.
iii. Maximum tensile and compressive stress in the beam results from sagging.
100 mm
20 mm
60 mm
120 mm
E E
5m
40 kN/m
y
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Q & A
Thank You….