 
			 
			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. | fx, τyx, τzx | 
| B. | τxx, τyx, u | 
| C. | τxx, τyx, τzx | 
| D. | τxx, p, τzx | 
| Answer» D. τxx, p, τzx | |
| 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=μ∇2v+ρg | 
| D. | 0=μ∇2v+ρg | 
| 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. | Γ | 
| B. | ρ | 
| C. | Φ | 
| D. | \(\vec{u}\) | 
| Answer» B. ρ | |