MCQOPTIONS
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This section includes 10 Mcqs, each offering curated multiple-choice questions to sharpen your Computational Fluid Dynamics knowledge and support exam preparation. Choose a topic below to get started.
| 1. |
To which of these flows, the Euler equation is applicable? |
| A. | Couette flow |
| B. | Potential flow |
| C. | Stokes Flow |
| D. | Poiseuille s flow |
| Answer» C. Stokes Flow | |
| 2. |
In Euler form of energy equations, which of these terms is not present? |
| A. | Rate of change of energy |
| B. | Heat radiation |
| C. | Heat source |
| D. | Thermal conductivity |
| Answer» E. | |
| 3. |
Which of the variables in the equation ( rho frac{Du}{Dt}=- frac{ partial p}{ partial x}+ frac{ partial tau_{xx}}{ partial x}+ frac{ partial tau_{yx}}{ partial y}+ frac{ partial tau_{zx}}{ partial z}+ rho f_x ) will become zero for formulating Euler equation? |
| A. | f<sub>x</sub>, <sub>yx</sub>, <sub>zx</sub> |
| B. | <sub>xx</sub>, <sub>yx</sub>, u |
| C. | <sub>xx</sub>, <sub>yx</sub>, <sub>zx</sub> |
| D. | <sub>xx</sub>, p, <sub>zx</sub> |
| Answer» D. <sub>xx</sub>, p, <sub>zx</sub> | |
| 4. |
Which of these equations represent a Euler equation? |
| A. | ( rho frac{Dv}{Dt}=- nabla p+ rho g ) |
| B. | ( rho frac{Dv}{Dt}=- nabla p+ mu nabla^2 v+ rho g ) |
| C. | p= <sup>2</sup>v+ g |
| D. | 0= <sup>2</sup>v+ g |
| Answer» B. ( rho frac{Dv}{Dt}=- nabla p+ mu nabla^2 v+ rho g ) | |
| 5. |
There is no difference between Navier-Stokes and Euler equations with respect to the continuity equation. Why? |
| A. | Convection term plays the diffusion term s role |
| B. | Diffusion cannot be removed from the continuity equation |
| C. | Its source term balances the difference |
| D. | The continuity equation by itself has no diffusion term |
| Answer» E. | |
| 6. |
Euler form of momentum equations does not involve this property. |
| A. | Stress |
| B. | Friction |
| C. | Strain |
| D. | Temperature |
| Answer» C. Strain | |
| 7. |
Eulerian equations are suitable for which of these cases? |
| A. | Compressible flows |
| B. | Incompressible flows |
| C. | Compressible flows at high Mach number |
| D. | Incompressible flows at high Mach number |
| Answer» E. | |
| 8. |
Which of these is the non-conservative differential form of Eulerian x-momentum equation? |
| A. | ( frac{ partial( rho u)}{ partial t}+ nabla.( rho u vec{V})=- frac{ partial p}{ partial x}+ rho f_x ) |
| B. | ( rho frac{Du}{Dt}=- frac{ partial p}{ partial x}+ rho f_x ) |
| C. | ( frac{( rho u)}{ partial t}=- frac{ partial p}{ partial x}+ rho f_x ) |
| D. | ( rho frac{ partial u}{ partial t}=- frac{ partial p}{ partial x}+ rho f_x ) |
| Answer» C. ( frac{( rho u)}{ partial t}=- frac{ partial p}{ partial x}+ rho f_x ) | |
| 9. |
Euler equations govern ____________ flows. |
| A. | Viscous adiabatic flows |
| B. | Inviscid flows |
| C. | Adiabatic and inviscid flows |
| D. | Adiabatic flows |
| Answer» D. Adiabatic flows | |
| 10. |
The general transport equation is ( frac{ partial( rho Phi)}{ partial t}+div( rho Phi vec{u})+div( Gamma grad Phi)+S ). For Eulerian equations, which of the variables in the equation becomes zero? |
| A. | |
| B. | |
| C. | |
| D. | ( vec{u} ) |
| Answer» B. | |