Finite Element Methods MCQs

Finite Element Methods MCQs

Try to answer these 90+ Finite Element Methods MCQs and check your understanding of the Finite Element Methods subject.
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1: Symmetry and sparsity of the global stiffness matrix can be approached by _____ methods.

A.   One

B.   Three

C.   Two

D.   Four

2: Which of these was one of the methods for determining assembly of the global stiffness matrix?

A.   Galerkin approach

B.   Skyline approach

C.   Rayleigh method

D.   Assembly method

3: In a banded matrix, elements are _____ placed in the stiffness matrix.

A.   Singular

B.   Determinant values

C.   Directly

D.   Indirectly

4: In Skyline matrix, the elements in a stiffness matrix can be placed in _______

A.   Direct values

B.   Determinant values

C.   Load values

D.   Vector form

5: The first step of skyline assembly matrix involves evaluation of ____

A.   Column height

B.   Row height

C.   Matrix height

D.   Undefined

6: The second step in skyline approach is assembling the element stiffness values into _____

A.   Row vector

B.   Identity vector

C.   Column vector

D.   Determinant vector

7: The details of a skyline assembly matrix are implemented in a program called ____

A.   Boolean program

B.   Cholesky program

C.   Truss program

D.   Trussky program

8: In 2D elements. Discretization can be done. The points where triangular elements meet are called ____

A.   Displacement

B.   Nodes

C.   Vector displacements

D.   Co-ordinates

9: Each triangle formed by three nodes and three sides is called a ______

A.   Node

B.   Force matrix

C.   Displacement vector

D.   Element

10: The finite element method is used to solve the problem ______

A.   Uniformly

B.   Vigorously

C.   Approximately

D.   Identically

11: In two dimensional modelling each node has ____ degrees of freedom.

A.   One

B.   Infinity

C.   Finite

D.   Two

12: The information of array of size and number of elements and nodes per element can be seen in ___

A.   Column height

B.   Element connectivity table

C.   Matrix form

D.   Undefined

13: Finite element method uses the concept of _____

A.   Nodes and elements

B.   Nodal displacement

C.   Shape functions

D.   Assembling

14: For constant strain elements the shape functions are ____

A.   Spherical

B.   Quadratics

C.   Polynomial

D.   Linear

15: Linear combination of these shape functions represents a ______

A.   Square surface

B.   Linear surface

C.   Plane surface

D.   Combinational surface

16: In particular, N 1+N 2 +N 3 represent a plane at a height of one at nodes ______

A.   One

B.   Two

C.   Three

D.   One, two and three

17: In two dimensional problems x-, y- coordinates are mapped onto ____

A.   X-, y- coordinates

B.   X-, ξ – co-ordinates

C.   η-, y- coordinates

D.   ξ-η-Co-ordinates

18: The shape functions are physically represented by _____

A.   Triangular coordinates

B.   ξ-,η-Co-ordinates

C.   Area coordinates

D.   Surface coordinates

19: The equation u=Nq is a _____ representation.

A.   Nodal

B.   Isoparametric

C.   Biparametric

D.   Co-ordinate

20: For plane stress or plane strain, the element stiffness matrix can be obtained by taking _____

A.   Shape functions, N

B.   Material property matrix, D

C.   Iso parametric representation, u

D.   Degrees of freedom, DoF

21: In the equation KQ=F, K is called as ____

A.   Stiffness matrix

B.   Modified stiffness matrix

C.   Singular stiffness matrix

D.   Uniform stiffness matrix

22: Principal stresses and their directions are calculated by using ____

A.   Galerkin approach

B.   Rayleigh method

C.   Potential energy method

D.   Mohr’s circle method

23: I the distribution of the change in temperature ΔT, the strain due to this change is ____

A.   Constant strain

B.   Stress

C.   Initial strain

D.   Uniform strain

24: Finite element method is used for computing _____ and _____

A.   Stress and strain

B.   Nodes and displacement

C.   Nodes and elements

D.   Displacement and strain

25: In deformation of the body, the symmetry of ______ and symmetry of ____ can be used effectively.

A.   Stress and strain

B.   Nodes and displacement

C.   Geometry and strain

D.   Geometry and loading

26: For a circular pipe under internal or external pressure, by symmetry all points move _____

A.   Radially

B.   Linearly

C.   Circularly

D.   Along the pipe

27: Boundary conditions can be easily considered by using _______

A.   Rayleigh method

B.   Penalty approach method

C.   Galerkin approach

D.   Potential energy approach

28: When dividing an area into triangles, avoid large _____

A.   Dimensions

B.   Loading

C.   Aspect ratios

D.   Boundary conditions

29: In dividing the elements a good practice may be to choose corner angles in the range of ____

A.   30-120°

B.   90-180°

C.   25-75°

D.   45-180°

30: Stresses can be change widely at ____

A.   Large circular sections

B.   Notches and fillets

C.   Corners

D.   Crystals

31: The Constant strain triangle can give____ stresses on elements.

A.   Linear

B.   Constant

C.   Uniform

D.   Parallel

32: The _____ can be obtained even with coarser meshes by plotting and extrapolating.

A.   Minimum stresses

B.   Minimum strain

C.   Maximum stresses

D.   Maximum strain

A.   Loading

B.   Notches and fillets

C.   Crystals

D.   Initial trails

34: Increasing the number of nodes in coarse mesh regions where stress variations are high, should give better results. This method is called _____

A.   Divergence

B.   Convergence

C.   Convergent- divergent

D.   Un defined

35: In two dimensional isoparametric elements, we can generate element stiffness matrix by using ____

A.   Numerical integration

B.   Differential equations

C.   Partial derivatives

D.   Undefined

36: For a four noded quadrilateral, we define shape functions on _____

A.   X direction

B.   Y direction

C.   Load vector

D.   Master element

37: The master element is defined in ______

A.   Co-ordinates

B.   Natural coordinates

C.   Universal coordinates

D.   Radius

38: The stiffness matrix from the quadrilateral element can be derived from _____

A.   Uniform energy

B.   Strain energy

C.   Stress

D.   Displacement

39: For four noded quadrilateral element, the global load vector can be determined by considering the body force term in _____

A.   Kinetic energy

B.   Potential energy

C.   Kinetic energy

D.   Temperature

40: Shape functions are linear functions along the _____

A.   Surfaces

B.   Edges

C.   Elements

D.   Planes

41: The stresses in the quadratic element are not ______

A.   Linear

B.   Uniform

C.   Constant

D.   Undefined

42: The stresses are evaluated at the __________

A.   Nodal points

B.   Nodal displacements

C.   Gauss points

D.   Elements

43: For quadrilaterals with 2X2 integration gives _____ sets of stress values.

A.   One

B.   Two

C.   Three

D.   Four

44: For degenerate four noded quadrilateral element the errors are _____

A.   Constant

B.   Uniform

C.   Higher

D.   Lesser

45: Gauss points are also the points used for numerical evaluation of _____ Surfaces

A.   K

B.   E

C.   Elements

D.   Planes

46: In the four-node quadrilateral element, the shape functions contained terms _________

A.   ξ

B.   σ

C.   C)

D.   ∅

47: A _________ element by using a nine-node shape function.

A.   Load vector

B.   Sub parametric

C.   Element displacement vector

D.   Constant matrix

48: Eight-Node Quadrilateral. This element belongs to the ________ family of elements.

A.   Serendipity

B.   Constant matrix

C.   Load vector

D.   Master element

49: Six node triangular elements is also known as _____

A.   Triangle

B.   Quadratic triangle

C.   Interpolation

D.   Shape function

50: In six node triangular element, the gauss points of a triangular element can be defined by ____

A.   Two point rule

B.   Three point rule

C.   One point rule

D.   Undefined