Explore topic-wise MCQs in Computational Fluid Dynamics Questions and Answers.

This section includes 6 Mcqs, each offering curated multiple-choice questions to sharpen your Computational Fluid Dynamics Questions and Answers knowledge and support exam preparation. Choose a topic below to get started.

1.

The formula to find ω from the k-value obtained using the turbulence intensity is ____________

A. ω=\(\frac{k^{3/2}}{l^2}\)
B. ω=\(\frac{k^{3/2}}{l}\)
C. ω=\(\frac{k^{1/2}}{l^2} \)
D. ω=\(\frac{k^{1/2}}{l}\)
Answer» E.
2.

The relationship between the turbulence intensity Ti and the turbulence kinetic energy k is given by ___________

A. k=\(\frac{1}{2}T_i(\vec{v}.\vec{v})\)
B. k=\(\frac{1}{2}T_i^2(\vec{v}.\vec{v})\)
C. k=\(\frac{1}{2}T_i^2(\vec{v}.\vec{v})\)
D. k=\(\frac{1}{2T_i}(\vec{v}.\vec{v})\)
Answer» C. k=\(\frac{1}{2}T_i^2(\vec{v}.\vec{v})\)
3.

Which of these is correct about the first internal node of a k-ε model?

A. k-equation is not solved
B. ε-equation is not solved
C. Both k and ε-equations are not solved
D. Both k and ε-equations are solved simultaneously
Answer» C. Both k and ε-equations are not solved
4.

When k and ε values are not available, for inlet boundary conditions, they are ____________

A. obtained from turbulence intensity
B. assumed to be zero
C. assumed to be unity
D. obtained from Reynolds number
Answer» B. assumed to be zero
5.

Boundary conditions near the solid-walls for a k-ε model depends on ___________

A. Eddy viscosity
B. Reynolds number
C. ε-value
D. k-value
Answer» C. ε-value
6.

If n is the spatial coordinate, in the outlet or symmetry boundaries, which of these following is correct for a k-ε model?

A. \(\frac{\partial k}{\partial n}=0; \frac{\partial\varepsilon}{\partial n}=0\)
B. \(\frac{\partial^2 k}{\partial n^2}=0; \frac{\partial\varepsilon}{\partial n}=0\)
C. \(\frac{\partial k}{\partial n}=0; \frac{\partial^2 \varepsilon}{\partial n^2}=0\)
D. \(\frac{\partial ^2 k}{\partial n^2}=0; \frac{\partial^2 \varepsilon}{\partial n^2}=0\)
Answer» B. \(\frac{\partial^2 k}{\partial n^2}=0; \frac{\partial\varepsilon}{\partial n}=0\)