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51.

The coefficient matrix in the global matrix format of the algebraic equations is a ______________(a) sparse matrix(b) dense matrix(c) diagonal matrix(d) symmetric matrixThe question was posed to me by my college professor while I was bunking the class.This interesting question is from Numerical Methods in chapter Numerical Methods of Computational Fluid Dynamics

Answer» CORRECT OPTION is (a) sparse matrix

To explain I would say: Each row in the coefficient matrix represents an equation corresponding to a single NODE. This equation contains coefficients of the neighbouring elements only depending on the element connectivity of the OWNER element. So, all other elements of that row BECOME zero. This makes the coefficient matrix sparse.
52.

Which of these creates a problem in Newton’s method for solving non-linear system of equations?(a) Taylor series(b) Jacobian(c) Convergence(d) SpeedThis question was posed to me during an internship interview.My query is from Numerical Methods in division Numerical Methods of Computational Fluid Dynamics

Answer»

The correct choice is (b) Jacobian

The BEST explanation: At each iteration of Newton’s METHOD, Jacobian has to be evaluated for the method to be EFFECTIVE. Evaluation of the Jacobian with n^2 ELEMENTS at each step will be expensive. MOREOVER, a direct method of evaluating the Jacobian does not exist.

53.

The number of operations for LU decomposition method is ____________ the number of operations for the Gauss elimination method.(a) twice(b) half of(c) one-third of(d) thriceThe question was asked in an interview for job.This key question is from Numerical Methods topic in section Numerical Methods of Computational Fluid Dynamics

Answer»

Correct option is (a) TWICE

To explain: LU decomposition is COMPUTATIONALLY more expensive than the Gauss elimination method. The number of operations INVOLVED is \(\frac{2N^3}{3}\). This is because the same PROCESS of Gauss elimination is carried out twice in the LU decomposition case.

54.

After the forward elimination step of the Gauss elimination method, the coefficient matrix is reduced to ____________(a) a lower triangular matrix(b) an upper triangular matrix(c) a diagonal matrix(d) a banded matrixThis question was addressed to me in a job interview.The origin of the question is Numerical Methods in portion Numerical Methods of Computational Fluid Dynamics

Answer»

The CORRECT answer is (b) an upper triangular matrix

For EXPLANATION I would say: After the forward ELIMINATION step, the main diagonal ELEMENTS and the elements above it are non-ZEROS. All the elements below the main diagonal are zeros. So, we can say that it gives an upper triangular matrix to be solved.

55.

Which of these direct methods is suitable only for banded matrices?(a) Gauss elimination(b) LU decomposition(c) PDMA(d) LU decomposition by Gauss eliminationI got this question in final exam.This interesting question is from Numerical Methods in section Numerical Methods of Computational Fluid Dynamics

Answer»

Correct choice is (c) PDMA

Easy explanation: PDMA stands for Penta-Diagonal MATRIX Algorithm. This is used for solving a Penta-diagonal matrix which has non-zero elements only in its MAIN diagonal and TWO DIAGONALS above and below it. A Penta-diagonal matrix is a sparse (fewer non-zero elements) banded matrix.

56.

The mathematical model is based on ____________(a) physical principles and assumptions(b) physical principles(c) flow model(d) flow model and assumptionsThe question was posed to me in unit test.My question comes from Numerical Methods topic in portion Numerical Methods of Computational Fluid Dynamics

Answer»

The correct OPTION is (a) physical principles and assumptions

To explain I would say: For GENERATING the mathematical model, first of all, the physical principles which are applicable to the given flow should be taken. Along with these some assumptions ALSO must be made to make the model suit the mathematical SOLUTION. These assumptions result in modelling errors.

57.

In incomplete Cholesky decomposition, the preconditioner matrix produced is ____________ (Note: L is the factorized lower triangular matrix and U is the factorized lower triangular matrix).(a) UL’(b) LU’(c) LL’(d) LL^2I got this question at a job interview.This intriguing question originated from Numerical Methods in section Numerical Methods of Computational Fluid Dynamics

Answer»

Right choice is (C) LL’

The explanation is: In incomplete Cholesky DECOMPOSITION, FACTORIZATION is done only for the lower triangular matrix and the preconditioner matrix is LL’. The coefficient matrix is also APPROXIMATELY equal to the preconditioner matrix.

58.

Which of these is an advantage of the Finite Difference Method over the Finite Volume Method?(a) Conservativeness(b) Higher-order(c) Stability(d) Complex problemsThis question was addressed to me in an interview.My question is taken from Numerical Methods in division Numerical Methods of Computational Fluid Dynamics

Answer»

Right answer is (b) HIGHER-order

Best explanation: The FINITE Volume METHOD cannot be APPLIED to higher ORDERS. The disadvantage of the Finite Volume Method, when compared to the Finite Difference Method, is that for orders higher than second order are more difficult to develop in 3-D.

59.

Which of these properties is not ensured in Finite Difference Methods?(a) Stability(b) Convergence(c) Conservativeness(d) AccuracyThe question was posed to me in exam.This interesting question is from Numerical Methods topic in division Numerical Methods of Computational Fluid Dynamics

Answer»

Right CHOICE is (c) Conservativeness

The explanation: Though the Finite Difference method is the easiest, it is suitable only for simple problems involving structured grids. Another main DISADVANTAGE is that conservation is not enforced UNLESS special care is taken.

60.

Each node has 4 nearest neighbours. This statement is correct for which of these grid types?(a) Structured 2-D grids(b) Unstructured 2-D grids(c) Structured 3-D grids(d) Unstructured 3-D gridsThis question was addressed to me by my school principal while I was bunking the class.This key question is from Numerical Methods in portion Numerical Methods of Computational Fluid Dynamics

Answer»

The correct answer is (a) Structured 2-D grids

The EXPLANATION: Structured grids have 2 nearest neighbours in 1-D, 4 in 2-D and 6 in 3-D. There is no standard number of nearest neighbours in the UNSTRUCTURED GRID TYPE except 1-D CASE where there is no option for the grids to have more than two neighbours.

61.

Which of these statements are wrong considering Control Volume based Finite Element Method?(a) Control volumes are formed(b) Integral form of the conservation equation is used(c) The centroid of the elements is used(d) Conservation equations are applied to the centroidsThe question was asked in an interview for internship.Question is from Numerical Methods topic in division Numerical Methods of Computational Fluid Dynamics

Answer»

Correct choice is (d) Conservation equations are applied to the CENTROIDS

The explanation is: In CV-FEM, control VOLUMES are formed by JOINING the centroids of the elements. The conservation equation in the INTEGRAL form is applied to these control volumes as in the FINITE Volume Method.

62.

To obtain the derivatives of the variables with respect to the coordinates, which of these approximations are used in the Finite Difference Method?(a) Taylor series and polynomial fitting(b) Fourier series and polynomial fitting(c) Taylor series and Fourier series(d) Taylor series and interpolationThis question was posed to me during an interview.This interesting question is from Numerical Methods topic in chapter Numerical Methods of Computational Fluid Dynamics

Answer»

Right choice is (a) Taylor series and polynomial fitting

The best I can EXPLAIN: The CONSERVATION equation of the partial differential FORM is used by the Finite DIFFERENCE METHOD. To approximate the derivatives in this equation, Taylor series and polynomial fitting are used.

63.

In a two-dimensional flow, the algebraic equation of an element relates the element with ___________(a) its face centres(b) its vertices(c) its faces(d) its neighboursI have been asked this question in examination.Question is taken from Numerical Methods in division Numerical Methods of Computational Fluid Dynamics

Answer»

The correct choice is (d) its neighbours

Easiest explanation: Each ELEMENT in a mesh has its own ALGEBRAIC equation. This algebraic equation has the coefficients of the NEIGHBOURING elements too. This WAY, the elements are connected to their neighbours by these algebraic EQUATIONS.

64.

While using a Finite Element Method, one has to approximate ____________(a) boundary conditions(b) integrals at grid faces(c) derivatives at grid points(d) shape functions and weighting functionsThis question was posed to me in unit test.The question is from Numerical Methods topic in chapter Numerical Methods of Computational Fluid Dynamics

Answer»

The correct option is (d) shape functions and weighting functions

Explanation: While using the FINITE Element Method for solving a problem, shape functions and weighting functions are APPROXIMATED. Integrals at GRID faces are approximated for Finite Volume METHODS. Derivatives at grid points are approximated for Finite Difference Methods.

65.

Express the 2-dimensional continuity equation in cylindrical coordinates.(a) \(\frac{\partial(\rho v_r)}{\partial r}+\frac{1}{r}\frac{\partial(\rho v_\theta)}{\partial\theta}+\frac{\rhov_r}{r}=0\)(b) \(\frac{\partial(\rho v_r)}{\partial r}+\frac{1}{r}\frac{\partial(\rho v_\theta)}{\partial\theta}+\rho\frac{v_r}{r}+\frac{\partial\rho}{\partial t}=0 \)(c) \(\frac{\partial(\rho v_r)}{\partial r}+\frac{1}{r}\frac{\partial(\rho v_\theta)}{\partial\theta}+\frac{\partial\rho}{\partial t}=0\)(d) \(\frac{\partial(\rho v_r)}{\partial r}+\frac{1}{r}\frac{\partial(\rho v_\theta)}{\partial\theta}+\rho \frac{v_r}{r}+\frac{\partial\rho}{\partial t}=0\)This question was addressed to me in an interview for internship.Question is taken from Numerical Methods in section Numerical Methods of Computational Fluid Dynamics

Answer»

The correct option is (b) \(\FRAC{\partial(\rho v_r)}{\partial r}+\frac{1}{r}\frac{\partial(\rho v_\theta)}{\partial\theta}+\rho\frac{v_r}{r}+\frac{\partial\rho}{\partial t}=0 \)

To explain I WOULD say: In Cartesian coordinates, RADIAL and angular velocities REPLACE the x and y velocity components. Similarly, (r, θ) is the COORDINATE system used here. The continuity equation in this system can be given by \(\frac{\partial(\rho v_r)}{\partial r}+\frac{1}{r}\frac{\partial(\rho v_\theta)}{\partial\theta}+\rho\frac{v_r}{r}+\frac{\partial\rho}{\partial t}=0 \).

66.

The multi-grid approach is a ___________ process.(a) direct(b) iterative(c) cyclic(d) periodicThis question was addressed to me in an internship interview.This intriguing question originated from Numerical Methods in chapter Numerical Methods of Computational Fluid Dynamics

Answer»

The correct answer is (C) cyclic

For explanation I WOULD say: The multi-grid approach involves TRAVERSAL from a FINE grid into a coarse ONE in order to make the error considerable and again another traversal from a coarse grid into a fine one after the error correction.

67.

Multi-grid approach switches between ___________ and ____________ grids to meet the errors.(a) structured and unstructured(b) collocated and staggered(c) cylindrical to polar(d) fine and coarseThis question was posed to me in a job interview.Asked question is from Numerical Methods topic in chapter Numerical Methods of Computational Fluid Dynamics

Answer»

Right choice is (d) fine and coarse

Easy EXPLANATION: The low frequency errors create problem in fine grids as the ERROR in ONE cell is very small and negligible because of the HIGH wavelength of the errors. So, multi-grid approach changes these fine grids into coarser one to MAKE it considerable in one cell.

68.

Which of these methods is not restricted to symmetric positive definite matrices?(a) The method of steepest descent(b) Conjugate gradient method(c) Bi-conjugate gradient method(d) Gauss-Seidel methodThe question was posed to me in homework.My question comes from Numerical Methods in chapter Numerical Methods of Computational Fluid Dynamics

Answer»

Right option is (d) Gauss-Seidel method

To explain I would SAY: The GRADIENT ITERATIVE solvers are restricted to SYMMETRIC positive definite matrices. The gradient methods are:

The method of Steepest descent

Conjugate gradient method

Bi-conjugate gradient method

Preconditioned bi-conjugate gradient method.

69.

Preconditioners improve ____________ of the coefficient matrix.(a) sparsity(b) rank(c) spectral properties(d) SingularityThis question was addressed to me in an internship interview.I need to ask this question from Numerical Methods in section Numerical Methods of Computational Fluid Dynamics

Answer» CORRECT CHOICE is (c) spectral properties

The best explanation: For a system of equations to have a better rate of convergence, the COEFFICIENT matrix should have a less spectral radius. So, Preconditioners are used to IMPROVE the spectral characteristics of a system to GIVE the same solution.
70.

In the boundary faces, the normal vector points _____________(a) to the owner element(b) outside the domain(c) in the direction of the flux(d) in the direction opposite to the fluxThe question was posed to me in my homework.I want to ask this question from Numerical Methods topic in portion Numerical Methods of Computational Fluid Dynamics

Answer» CORRECT choice is (b) OUTSIDE the domain

Explanation: The boundary FACES bound only ONE element and they do not have any neighbouring elements. So, the owner elements in the boundaries have their faces with the normal VECTORS pointing outside the domain.
71.

Consider the global matrix AΦ=b. If my coefficient matrix A is the same for different b vectors, which of these methods is economic?(a) Gauss elimination(b) TDMA(c) LU decomposition(d) PDMAI have been asked this question during an online exam.My question is based upon Numerical Methods in section Numerical Methods of Computational Fluid Dynamics

Answer»

Correct option is (c) LU decomposition

The EXPLANATION is: Once matrix A is factorized in the LU decomposition method, the same factorized MATRICES can be used to SOLVE DIFFERENT b vectors. Because decomposition does not depend upon the b vector. This is the MAJOR advantage of the LU decomposition method.

72.

If N is the number of unknowns, the number of operations required for backward substitution is ____________(a) \(\frac{N^3}{3}\)(b) \(\frac{N^3}{2}\)(c) \(\frac{N^2}{2}\)(d) \(\frac{N^2}{3}\)I had been asked this question during an interview.Query is from Numerical Methods in portion Numerical Methods of Computational Fluid Dynamics

Answer»

Correct CHOICE is (C) \(\frac{N^2}{2}\)

BEST explanation: The number of operations required for the overall Gauss elimination method is \(\frac{N^3}{3}\). The number of operations for backward SUBSTITUTION is \(\frac{N^2}{2}\). This high computational cost is the DISADVANTAGE of the Gauss elimination method.

73.

Curvilinear coordinates do not suit __________(a) Unstructured grids(b) Structured grids(c) Orthogonal grids(d) Non-orthogonal gridsThe question was posed to me during an interview for a job.This interesting question is from Numerical Methods in division Numerical Methods of Computational Fluid Dynamics

Answer»

The CORRECT answer is (a) Unstructured grids

To explain I would say: For curvilinear COORDINATES, the grid should be very smooth and the change of grid direction from point to point must be very small. Since the grid direction in the unstructured grids varies MUCH, they do not suit unstructured grids.

74.

Conservation of Finite Volume Method depends on ___________(a) surface integrals(b) volume integrals(c) convection(d) diffusionThe question was posed to me during an online exam.The origin of the question is Numerical Methods in section Numerical Methods of Computational Fluid Dynamics

Answer»

Right option is (a) SURFACE integrals

The explanation: The Finite VOLUME METHODS are CONSERVATIVE as long as the surface integrals which represent the convective and diffusive fluxes are the same for two control volumes sharing the same boundary.

75.

Which of these coordinates are not used in CFD?(a) Orthogonal coordinates(b) Cartesian coordinates(c) Spherical coordinates(d) Number lineThe question was posed to me in an international level competition.The query is from Numerical Methods in portion Numerical Methods of Computational Fluid Dynamics

Answer» CORRECT ANSWER is (d) Number line

To elaborate: The type of COORDINATE system can be opted between Cartesian, CYLINDRICAL, Spherical, Curvilinear orthogonal and non-orthogonal. A Number line cannot be used as a coordinate system in CFD.
76.

Which of these points is shared by the maximum number of elements?(a) Grid point(b) Cell centre(c) Face centre(d) VertexThis question was posed to me in an online interview.This interesting question is from Numerical Methods in chapter Numerical Methods of Computational Fluid Dynamics

Answer»

The CORRECT answer is (d) Vertex

For explanation: A vertex is shared by the most number of elements. In structured grids, a vertex POINT is shared by eight elements. Gridpoint can be EITHER the cell centre or the vertex depending UPON the TYPE of discretization.