 
			 
			MCQOPTIONS
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				This section includes 9 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. | Along the downwind line of the NVD, the values of _____________ are changed to make the system stable. | 
| A. | ac | 
| B. | (l,k) | 
| C. | Φc | 
| D. | Φf | 
| Answer» C. Φc | |
| 2. | What is DWFf for the second-order upwind scheme? | 
| A. | \(\frac{\tilde{\phi_c}}{2(1-\tilde{\phi_c})}\) | 
| B. | \(\frac{1}{2(1-\tilde{\phi_c})}\) | 
| C. | \(\frac{\tilde{\phi_c}}{4(1-\tilde{\phi_c})}\) | 
| D. | \(\frac{1}{4(1-\tilde{\phi_c})}\) | 
| Answer» B. \(\frac{1}{2(1-\tilde{\phi_c})}\) | |
| 3. | The deferred correction source term of the NWF method using he normalized interpolation profile \(\tilde{\phi_f}=l\tilde{\phi_c}+k\) is _________ | 
| A. | (1-l-k)Φu | 
| B. | (k)Φu | 
| C. | (-l)Φu | 
| D. | (l-k)Φu | 
| Answer» B. (k)Φu | |
| 4. | The value of DWFf for the central difference scheme is __________ | 
| A. | 1 | 
| B. | \(\frac{1}{3}\) | 
| C. | \(\frac{1}{4}\) | 
| D. | \(\frac{1}{2}\) | 
| Answer» E. | |
| 5. | For a scheme modelled using the DWF method, the diagonal coefficient becomes zero when ___________ | 
| A. | DWFf > 0 | 
| B. | DWFf > 1 | 
| C. | DWFf > 0.5 | 
| D. | DWFf > 2 | 
| Answer» D. DWFf > 2 | |
| 6. | DWFf for the FROMM scheme is ___________ | 
| A. | \(\frac{1}{2(1-\tilde{\phi_c})}\) | 
| B. | \(\frac{1}{4(1-\tilde{\phi_c})}\) | 
| C. | \(\frac{1}{2}\) | 
| D. | \(\frac{1}{4}\) | 
| Answer» C. \(\frac{1}{2}\) | |
| 7. | The value of DWF for the downwind scheme is __________ | 
| A. | 0 | 
| B. | 1 | 
| C. | 2 | 
| D. | 3 | 
| Answer» C. 2 | |
| 8. | The value of the Downwind Weighing Factor (DWF) lies between ___________ | 
| A. | 0≤DWF≤∞ | 
| B. | DWF≥0 | 
| C. | 0≤DWF≤1 | 
| D. | DWF≤1 | 
| Answer» D. DWF≤1 | |
| 9. | The Downwind Weighing Factor in the normalized form is given by __________ | 
| A. | \(\frac{\tilde{\phi_f}-\tilde{\phi_c}}{1-\tilde{\phi_c}}\) | 
| B. | \(\frac{\tilde{\phi_c}-\tilde{\phi_f}}{1-\tilde{\phi_c}}\) | 
| C. | \(\frac{\tilde{\phi_f}-\tilde{\phi_c}}{1-\tilde{\phi_f}}\) | 
| D. | \(\frac{\tilde{\phi_c}-\tilde{\phi_f}}{1-\tilde{\phi_f}}\) | 
| Answer» B. \(\frac{\tilde{\phi_c}-\tilde{\phi_f}}{1-\tilde{\phi_c}}\) | |