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This section includes 10 Mcqs, each offering curated multiple-choice questions to sharpen your Aerodynamics knowledge and support exam preparation. Choose a topic below to get started.
1. |
If a cone with half angle 30.2 degrees is kept in a flow at Mach number 3.5, then what is the value of Mach number downstream of the shockwave? |
A. | 1.110 |
B. | 2.482 |
C. | 1.648 |
D. | 3.45 |
Answer» D. 3.45 | |
2. |
The flow properties remain constant in a conical flow over which of the following? |
A. | Ray from a vertex |
B. | Along the axis |
C. | Along the conical base |
D. | Interior of the conical surface |
Answer» B. Along the axis | |
3. |
What happens to the velocity downstream of the shock as the deflection angle increases? |
A. | Remains same |
B. | Increases |
C. | Decreases |
D. | Tends to infinity |
Answer» D. Tends to infinity | |
4. |
What information does the shock polar provide? |
A. | Oblique shock properties |
B. | Normal shock properties |
C. | Shock angle |
D. | Intensity of shock |
Answer» B. Normal shock properties | |
5. |
What is the shape of the shock wave formed over a cone in a supersonic flow? |
A. | Normal shock |
B. | Conical shock |
C. | Straight shock |
D. | Triangular shock |
Answer» C. Straight shock | |
6. |
What is the application of studying conical flow? |
A. | Re-entry shuttle |
B. | Boeing A 320 |
C. | Flow over flat plate in wind tunnel |
D. | Hot air balloon |
Answer» B. Boeing A 320 | |
7. |
For a wedge and cone of same half angle, the shock wave formed at the cone is weaker. |
A. | True |
B. | False |
Answer» B. False | |
8. |
3D relieving effect is a consequence of which of these flows? |
A. | Flow over a wedge |
B. | Flow over a flat plate |
C. | Flow over a cone |
D. | Flow over a flat plate kept at 90 degrees |
Answer» D. Flow over a flat plate kept at 90 degrees | |
9. |
The flow stream behind the shock in a conical flow is parallel to the conical surface. |
A. | True |
B. | False |
Answer» C. | |
10. |
Conical flow is an example of which of these flows? |
A. | Axisymmetric flow |
B. | Two dimensional flow |
C. | Flow symmetrical about x z plane |
D. | One dimensional flow |
Answer» B. Two dimensional flow | |