81-01. Low Speed Aerodynamics
All questions: 645
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1. If velocity and angle of attack is kept constant and den sity decreases, the lift:
2. How is the thickness of an aerofoil section measured?
3. For a given angle of attack the lift/drag ratio:
4. When flaps are extended in a straight and level flight at constant IAS, the lift coefficient will eventually:
5. An aircraft at an IAS of 150 kts at sea level, then flies at 10.000 ft, the drag will:
