

MCQOPTIONS
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This section includes 3 Mcqs, each offering curated multiple-choice questions to sharpen your Aerodynamics knowledge and support exam preparation. Choose a topic below to get started.
1. |
Is boundary condition is applied at the control point? |
A. | False |
B. | True |
Answer» C. | |
2. |
Why source strength X per unit length is constant over a given panel? |
A. | It allows it to varies from one panel to next panel |
B. | It does not allow it to varies from one panel to next panel |
C. | It remains in the same panel |
D. | The length will be changes from panel to panel |
Answer» B. It does not allow it to varies from one panel to next panel | |
3. |
Is complete velocity potential at point p is obtained by entire source sheet from a to b? |
A. | True |
B. | False |
Answer» B. False | |