InterviewSolution
This section includes InterviewSolutions, each offering curated multiple-choice questions to sharpen your knowledge and support exam preparation. Choose a topic below to get started.
| 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 |
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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. |
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| 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 |
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Answer» The correct choice is (b) Jacobian |
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| 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 |
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Answer» Correct option is (a) TWICE |
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| 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 |
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Answer» The CORRECT answer is (b) an upper triangular matrix |
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| 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 |
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Answer» Correct choice is (c) PDMA |
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| 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 |
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Answer» The correct OPTION is (a) physical principles and assumptions |
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| 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 |
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Answer» Right choice is (C) LL’ |
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| 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 |
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Answer» Right answer is (b) HIGHER-order |
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| 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 |
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Answer» Right CHOICE is (c) Conservativeness |
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| 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 |
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Answer» The correct answer is (a) Structured 2-D grids |
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| 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 |
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Answer» Correct choice is (d) Conservation equations are applied to the CENTROIDS |
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| 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 |
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Answer» Right choice is (a) Taylor series and polynomial fitting |
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| 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 |
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Answer» The correct choice is (d) its neighbours |
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| 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 |
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Answer» The correct option is (d) shape functions and weighting functions |
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| 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 |
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Answer» The correct option is (b) \(\FRAC{\partial(\rho v_r)}{\partial r}+\frac{1}{r}\frac{\partial(\rho v_\theta)}{\partial\theta}+\rho\frac{v_r}{r}+\frac{\partial\rho}{\partial t}=0 \) |
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| 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 |
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Answer» The correct answer is (C) cyclic |
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| 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 |
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Answer» Right choice is (d) fine and coarse |
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| 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 |
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Answer» Right option is (d) Gauss-Seidel method |
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| 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 |
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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. |
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| 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 |
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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. |
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| 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 |
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Answer» Correct option is (c) LU decomposition |
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| 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 |
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Answer» Correct CHOICE is (C) \(\frac{N^2}{2}\) |
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| 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 |
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Answer» The CORRECT answer is (a) Unstructured grids |
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| 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 |
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Answer» Right option is (a) SURFACE integrals |
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| 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 |
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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. |
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| 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 |
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Answer» The CORRECT answer is (d) Vertex |
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