6th semester b.e. / b.tech
TRANSCRIPT
SEM-6 6th
Semester – B.E. / B.Tech.
BR-114
Department of Mechanical Engineering
ME86
92 Finite Element Analysis
Part-A (10 x 2 = 20 Marks)
UNIT – I
No Question Level Competence Mark
1.1 What are the types of boundary condition? L1 Understanding 2
1.2 Mention the basic steps of Rayleigh-Ritz method L2 Remembering 2
1.3 Name any four FEA software‟s L1 Evaluating 2
1.4 What is meant by Finite Element modeling? L2 Understanding
2
1.5 Mention the basic steps of Rayleigh-Ritz method? L3 Remembering 2
1.6 State the methods of Engineering analysis L4 Analyzing 2
1.7 What is meant by Finite element? L5 Understanding 2
1.8 What is meant by node or joint? L1 Understanding 2
1.9 Define shape functions. L1 Evaluating 2
1.10 What is meant by higher order elements? L2 Understanding 2
2.1 Name the variational methods. L1 Remembering 2
2.2 Give examples for the finite element. L2 Remembering 2
2.3 State the three phases of finite element method. L5 Remembering 2
2.4 Name the weighted residual methods. L3 Evaluating 2
Nadar Saraswathi College of Engineering and Technology,
Vadapudupatti, Theni - 625 531
(Approved by AICTE, New Delhi and Affiliated to Anna University, Chennai)
Format No. NAC/TLP-07a
Rev. No. 03
Date 29-11-2019
Total Page 01
Question Bank for the Units – I to V
2.5 What is truss element? L4 Understanding 2
2.6 What is “Aspect ratio”? L1 Understanding 2
2.7 List the two advantages of post-processing. L6 Remembering 2
2.8 What are structural and non-structural problems? L4 Understanding 2
2.9 Explain force method and stiffness method? L4 Understanding 2
2.10 What is the difference between static and dynamic
analysis?
L4 Analyze 2
3.1 What are types of loading acting on the structure? L4 Understanding 2
3.2 Define body force (f). L2 Remembering 2
3.3 What is point load (P). L4 Analyze 2
3.4 State the properties of a stiffness matrix. L5 Analyze 2
3.5 What is truss? L2 Understanding 2
3.6 Define heat transfer. L3 Remembering 2
3.7 Define Dynamic analysis. L3 Remembering 2
4.1 What are types of Eigen value problems? L6 Understanding 2
4.2 What are methods used for solving transient vibration
problems?
L4 Analyze 2
4.3 State the principles of virtual work. L4 Analyze 2
4.4 Define transaction force(T). L6 Remembering 2
4.5 What is the classification of Co-ordinates? L5 Understanding 2
4.6 Give the generations L4 Analyze 2
4.7 What are methods used for solving transient
problems?
L1 Understanding 2
5.1 How do you define two dimensional elements? L4 Analyze 2
5.2 What is CST element? L5 Understanding 2
5.3 What is LST element? L4 Understanding 2
5.4 What is QST element? L3 Understanding 2
5.5 What is meant by plain stress analysis? L1 Understanding 2
5.6 What is meant by plain stress analysis? L1 Understanding 2
5.7 Write a displacement function equation for CST
element.
L1 Understanding 2
5.8 State the assumption in the theory of pure torsion. L4 Analyze 2
6.1 Write down the finite element for tensional triangular
element.
L4 Analyze 2
6.2 Write down the shape function for two-dimensional
transfer.
L4 Analyze 2
6.3 Define path line. L1 Remembering 2
6.4 Define stream line. L1 Remembering 2
6.5 Write down the expression for stiffness matrix in two-
dimensional heat conduction and convection.
L2 Evaluating 2
6.6 Write down the governing equation for two
dimensional heat conduction.
L4 Analyze 2
6.7 Write down the stiffness matrix equation for one
dimensional heat transfer conduction element.
L4 Analyze 2
7.1 What is axisymmetric element? L4 Understanding 2
7.2 What ate the conduction for a problem to be
axisymmetric?
L2 Understanding 2
7.3 Write down the displacement equation for an
axisymmetric triangular element.
L4 Analyze 2
7.4 Give the stiffness matrix equation for an axisymmetric
triangular element.
L1 Remembering 2
7.5 What are the advantages of shell element? L2 Understanding 2
7.6 What are the assumption used in thick plate element? L1 Understanding 2
7.7 What are the assumption used in thin plate element? L2 Understanding 2
8.1 What are the ways in which a three dimensional
problem can be reduced to a two dimensional
approach?
L2 Understanding 2
8.2 Write down the stress-strain relationship for an
axisymmetric triangular element.
L4 Analyze 2
8.3 Give the strain-Displacement matrix for an
axisymmetric triangular element.
L1 Remembering 2
8.4 Define plate element. L1 Remembering 2
8.5 What are the assumptions for thin shell theory? L4 Analyze 2
8.6 Define dynamic analysis. L3 Remembering 2
8.7 Define normal modes. L3 Remembering 2
9.1 What is the purpose of Isoparametric element. L1 Understanding 2
9.2 Write down the shape function for 4 noded
rectangular elements using natural co-ordinate system.
L4 Analyze 2
9.3 Write down the jacobian matrix for four noded
quadrilateral element.
L4 Analyze 2
9.4 Write down the stiffness matrix equation for four
noded isoparametric quadrilateral element.
L3 Evaluating 2
9.5 Write down the element force vector equation for four
noded quadrilateral element.
L4 Analyze 2
9.6 Write down the Gaussian quadrature expression for
numerical integration.
L1 Evaluating 2
9.7 Define streamline. L2 Remembering 2
10.1 Define the stream function for a two dimensional
incompressible flow.
L2 Remembering 2
10.2 Define element capacitance matrix for unsteady state
transfer problem.
L2 Remembering 2
10.3 List the method of describing motion of fluid. L3 Remembering 2
10.4 Mention two natural boundary conditions as applied to
thermal problems.
L5 Evaluating 2
10.5 Define resonance. L1 Remembering 2
10.6 What are methods used for solving transient vibrations
problems?
L2 Understanding 2
10.7 Define linear dependence and independence of
vectors.
L3 Remembering 2
10.8 What are the types of Eigen value problems? L1 Understanding 2
10.9 What are the types of non-linearity? L2 Understanding 2
10.10 Is beam element an isoparametric element? L3 Evaluating 2
Part – B ( 5 x 13 = 65 Marks)
UNIT- I
11.a-1 The following differential equation is available for a
physical phenomenon, d2y/dx
2 – 10x
2 =5, 0≤x≤1 with
boundary conditions as y (0) = 0 and y (1) = 0.Find
L1 Knowledge
(13)
an approximate solution of the above differential
equation by using Galerkin‟s method of weighted
residuals and also compare with exact solution.
11.a-2 Solve differential equation for a physical problem
expressed as d2y/dx
2)+100=0, 0< x< 10 with Boundary
condition as y(0)=0, y(10)=0. using
(i)Point collocation (ii) Subdomain collocation
(iii) Least squares
(iv)Galerkin‟s method
L4 Analyzing (13)
11.a-3 Solve differential equation for a physical problem
expressed as d2y/dx
2)+60=0, 0< x< 10 with Boundary
condition as y(0)=0, y(10)=0. Trial function y=a1x(10-
x)using
(i)Point collocation (ii) Subdomain collocation
(iii) Least squares
(iv)Galerkin‟s method.
L3 Applying (13)
11.b-1 The differential equation of a physical phenomenon is
given by (d2y/dx
2)+500x
2=0, 0< x< 1 Trial Function,
y=a1(x-x4).Boundary condition are y(0)=0, y(1)=0.
Calculate the value of the parameter a1 by the
following methods:
(i)Point collocation (ii) Subdomain collocation
(iii) Least squares
(iv)Galerkin‟s
L4 Analyzing (13)
11.b-2 A beam AB of span „l‟ simply supported at the ends
and carrying a concentrated load „W‟ at the centre „C‟.
Determine the deflection at the mid span by using
Rayleigh-Ritz method and compare with exact
solution.
L4 Analyzing (13)
11.b-3 A simply Supported beam subjected to uniformly
distributed load over entire span it is subjected to a
point load at the centre of the span. Calculate the
deflection using Rayleigh-Ritz method and compare
with exact solutions
L4
Applying (13)
11.b-4 Determine the expression for deflection and bending
moment in a simply supported beam subjected to uniformly
distributed load over entire span. Find the deflection and
moment at mid span and compare with exact solution
Rayleigh-Ritz method. Use
L4 Applying
(13)
UNIT- II
12.a-1 A steel bar of length 800mm is subjected to an axial load of
3kN as shown in fig. Estimate the nodal displacement of
the bar and load vectors.
L4 Applying (13)
12.a-2 For a tapered bar of uniform thickness t=10mm as
shown in figure. Predict the displacements at the
nodes by forming into two element model. The bar
has a mass density ρ = 7800 Kg/m3, the young‟s
modulus E = 2x105
N/mm2. In addition to self-weight,
the bar is subjected to a point load P= 10 KN at its
centre. Also determine the reaction forces at the
support.
L1 Applying (13)
12.a-3 Consider a bar as shown in fig. Young‟s Modulus E= 2 x
105 N/mm
2. A1 = 2cm
2, A2 = 1cm
2 and force of 100N.
Calculate the nodal displacement.
L1 Applying (13)
12.a-4 For the two bar truss shown in the fig, Estimate the
displacements of node 1 and the stress in element 1-3.
L3 Applying (13)
12.b-1 Consider a three bar truss as shown in Fig.It is given that
E=2X105N/mm
2.Calculate the following.
(i) Nodal Displacement
(ii) Stress in each member.
(iii) Reaction at the support.
L3 Applying (13)
Take Area of element(1)=2000mm2
Area of element(2)=2500mm
2
Area of element(3)=2500mm
2
12.b-2 Consider a four bar as shown in Fig.It is given that
E=2X105N/mm
2 and Ae=625 mm
2 for all elements.
(i) Determine the element stiffness matrix for
each element.
(ii) Assemble the structure stiffness matrix K for
the entire truss.
(iii) Solve for the nodal displacement.
L3 Applying (13)
12.b-3 For the plane truss shown in Fig. Determine the
horizontal and vertical displacement of nodel and
stress in each element. All element have E=201GPa
and A=4X10-4
m2
L5
Applying (13)
12.b-4 For the three-bar truss shown in Fig. Determine the
displacement of node 1 and the stress in element 3
L1 Knowledge
(13)
UNIT- III
13.a-1 Calculate the element stiffness matrix and temperature
force vector for the plane stress element shown in fig.
The element experiences a 20ºC increase in
temperature. Assume α= 6x10^-6 C. Take E=2x10^5
N/mm2, v= 0.25, t= 5mm
L4 Analyzing (13)
13.a-2 Determine the shape function N1,N2 and N3 at the
interior point P for the triangular element shown in
Fig.
L4 Analyzing (13)
13.a-2 Determine the stiffness matrix for the constant strain
triangular (CST) element shown in Fig.The Co-
Ordinates are the given in units of mm. Assume plain
stress conditions. Take E=210GPa v=0.25 and
t=10mm.
L1 Knowledge
(13)
13.a-3 For the two dimensionalloaded plate shown in fig.
Determine the nodal displacement and element stress
using plane strain condition considering body force.
Take Young‟s modulus as 200Gpa, r=0.3 and density
as 7800kg/3m3.
L1 Knowledge (13)
13.a-4 Determine the nodal displacement of nodes 1 and 2
and element stress for the two dimentional loaded
plate as shown in Fig.Assume plane stress
L4 Analyzing (13)
condition.Take v=0.25,E= E=2x10^5 N/mm2, t=15mm
13.b-1 Find the temperature distribution in a square region
with uniform energy generation as shown in
Fig.Assume that there is no temperature variations in
thez-direction.Takek=30w/cmoc,l=10cm,
q=100w/cm3.
L3 Knowledge
(13)
13.b-2 A thin plate subjected to surface traction as shown in
Fig. Calculate the global stiffness matrix.Take
t=25mm, E=2x10^5 N/mm2,v=0.30,Assume the plain
stress condition.
L1 Knowledge (13)
13.b-3 Derive the shape functions for a constant strain
triangular (CST) element in terms of natural Co-
ordinate system.
L1 Knowledge (13)
UNIT- IV
14.a-1 The nodal coordinates for an axisymmetric triangular
element shown in fig are given below. Evaluate the strain-
displacement matrix for that element.
L1 Knowledge
(13)
14.a-2 Calculate the stiffness matrix for the axisymmetric element
shown in fig E= 2.1 x 106 N/mm
2 and Poisson‟s ratio as
0.3.
L4 Analyzing (13)
14.a-3 For the element shown in Fig,determine the sfiffness
matrix.Take E=200Gpa and v=0.25
L3 Apply
(13)
14.b-1 For the axisymmetric element shown in Fig.determine
the element streses.Take E= 2.1 x 106
N/mm2
and
v=0.25.The co-ordinates shown in Fig(i) are in
mm.The nodel displacement are,
u 1=0.05,u2=0.02,u3=0,w1=0.03,w2=0.02,w3=0
L4 Analyzing (13)
14.b-2 Calculate the element stiffness matrix and the thermal
force vector for the axisymmetric triangular element
shown in Fig. The experience a 15oc increase in
temperature.
L4 Analyzing (13)
14.b-3 For the axisymmetric element shown in Fig.
Determine the element stresses.Let E=210Gpa and
v=0.25.The co-ordinates in mm are shown in Fig.
u 1=0.05,u2=0.02,u3=0,w1=0.03,w2=0.02,w3=0
L3 Apply (13)
UNIT- V
15.a-1 Calculate the Cartesian coordinates of the point P which
has local coordinates ε = 0.8 and η = 0.6 as shown in figure
L4 Analyzing (13)
15.a-2 For the isoparametric four noded quadrilateral element
shown in Fig.Determine the Cartesian co-ordinates of
point P which has local co-ordinates ε = 0.5 and η =
0.5
L4 Analyzing (13)
15.a-3 For the isoparametric quadrilateral element shown in
Fig.determine the co=ordinate of the point P which
has Cartesian Co-ordinates (7,4)
L3 Apply (13)
15.b-1 Evaluate [J]= η=1/2 for the linear quadrilateral
element shown in Fig.
L4 Analyzing (13)
15.b-2 For four noded rectangular element is shown in Fig.
Determine the following:
1.Jacobian Matrix 2.Strain-Displacement matrix
3.Element Stresses .
L1 Knowledge (13)
15.b-3 Evaluate the Jacobian matrix for the isoparametric
quadrilateral element shown in Fig
L4 Analyzing (13)
15.b-4 For the isoparametric quadrilateral element shown in
Fig. The Cartesian co-ordinates of point P are
(6,4).The loads 10Kn and 12kN are acting in x and y
direction on that point P. Evaluate the nodal
equivalent forces.
L3 Apply (13)
Part – C ( 1 x 15 = 15 Marks)
UNIT-I
16 .a-1 What are the steps involved in FEA . L5 Evaluation (15)
16 .a-2 Explain the discretization process. L5 Evaluation (15)
(OR)
16.b-1 Explain the Following:
(i) Variational approach
(ii) Weighed residual methods.
L5 Evaluation (15)
16.b-2 What are the steps involved in Analysis Process. L5 Evaluation (15)
UNIT-II
16 .a-1 The composite structure shown in Fig., is subjected to
a bar element. Determine the displacement, stresses
and support reaction. Assume the following data:
L5 Evaluation (15)
16 .a-2 An aluminum alloy fin of 7 mm thick and 50mm long
protrudes from a wall, which is maintained at 120o
c.
The air temperature is 220
c. The heat transfer
coefficient and thermal conductivity of the fin
material ARE 140W/m2K and 55W/m
2K respectively.
Determine the temperature distribution of Fin.
L5 Evaluation (15)
(OR)
16.b-1 Consider the bar shown in figure axial force P =
100KN is applied as shown. Determine the nodal
displacement, stresses in each element and reaction
forces.Young‟sModulus. E=2x10^5 N/mm2.
A1=2cm2A2=1cm
2
L5 Evaluation (15)
16.b-2 Define Finite element modelling. L5 Evaluation (15)
UNIT-III
16 .a-1 A composite wall consists of three material as shown
in Fig. The outer temperature is T0=200C.convective
heat transfer takes place on the inner surface of wall
with Tα=8000C and h=75W/m
2 0c.Determine the
temperature distribution in the wall.
L5 Evaluation (15)
16.a-2 Assemble the Stain-Displacement matrix for the CST
element shown in Fig.Take t=25mm and E210Gpa.
L5 Evaluation (15)
(OR)
16.b-1 Evaluate the stiffness matrix for the CST shown in
Fig. Assume plane stress condition.Take t=20mm,
E=2x10^5 N/mm2,t=0.25.
L5 Evaluation (15)
16.b-2 What is CST and LST element? L5 Evaluation (15)
UNIT-IV
16 .a-1 The nodal co-ordinates for an axisymmetric triangular
element are given below:
r 1= 5mm,z1=15mm,r2=25mm,z2=15,r3=35mm,z3=50
mm, Determine [B] matrix for that element.
L5 Evaluation (15)
16.a-2 What are the ways in which a three dimensional
problem can be reduced to a two dimensional
approach?
L5 Evaluation (15)
(OR)
16.b-1 What is the assumption for thin shell theory? L5 Evaluation (15)
16.b-2 What is the assumption used in thick plate element?
And advantages of shell elements?
L5 Evaluation (15)
UNIT-V L5 Evaluation
16 .a-1 Define FEA software packages? L5 Evaluation (15)
16.a-2 Define the following terms with suitable exambles
(i) Isoparametric element
(ii) Axisymmetric analysis
(iii)Node, Element and shape functions
(iv) Plane stress and plane strain
L5 Evaluation (15)
(OR) L5 Evaluation
16.b-1 Define Natural Co-Ordinates? L5 Evaluation (15)
16.b-2 Define Solution Technique to Dynamic Problems. L5 Evaluation (15)
L1: Knowledge, L2: Comprehension, L3: Application, L4: Analysis, L5: Evaluation, L6: Synthesis
QUESTION BANK SUMMARY
S.NO UNIT DETAILS L1 L2 L3 L4 L5 L6 TOTAL
1 Unit-1
PART-A 6 4 2 5 2 1 20
PART-B 01 0 01 05 0 0 07
PART-C 0 0 0 0 03 0 03
2 Unit-2
PART-A 01 02 02 05 02 02 14
PART-B 02 0 03 01 01 0 07
PART-C 0 0 0 0 04 0 04
3 Unit-3
PART-A 05 01 01 07 01 0 15
PART-B 03 0 01 03 0 0 07
PART-C 0 0 0 0 04 0 04
4 Unit-4
PART-A 04 04 02 04 0 0 14
PART-B 01 0 02 03 0 0 06
PART-C 0 0 0 0 04 0 04
5 Unit-5
PART-A 04 05 04 03 01 0 17
PART-B 01 0 02 04 0 0 07
PART-C 0 0 0 0 04 0 04
Total No of Questions
PART-A PART-B PART-C TOTAL
80 34 19 133
Prepared By:
Staff Name1: Mr.V.Thirumalai raj Staff Name2:Mr.P.Surulimani