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November 1, 2016 by
EASA Module 8 : Basic Aerodynamics Questions
1. A delta wing has
2. The Lift/Drag ratio of a wing at the stalling angle is
3. The airflow over the upper surface of a cambered wing
4. The speed of air over a swept wing which contributes to the lift is
5. In straight and level flight, the angle of attack of a swept wing is
6. Induced drag
7. A delta wing aircraft flying at the same speed (subsonic) and angle of attack as a swept wing aircraft of similar wing area will produce
8. The stagnation point is
9. If a swept wing stalls at the tips first, the aircraft will
10. The thickness/chord ratio of the wing is also known as
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