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This section includes 2 Mcqs, each offering curated multiple-choice questions to sharpen your Aerodynamics Questions and Answers knowledge and support exam preparation. Choose a topic below to get started.
1. |
Flow separation causes lift to decrease with increasing angle of attack. This is inconsistent with the thin airfoil theory where the lift curve slope is 2π. This is a contradiction. |
A. | True |
B. | False |
Answer» C. | |
2. |
The d’Alembert’s Paradox is concerned with ____ |
A. | Lift arising due to pressure distribution |
B. | High viscous effects |
C. | Drag being zero for non-zero lift |
D. | Kutta condition not satisfied |
Answer» D. Kutta condition not satisfied | |