Aircraft Systems and Avionics: Key Concepts and Technologies
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Normal shock wave leads - to total turbulence behind shock wave
How to calculate drag coefficient - ratio between drag pressure to dynamic pressure
Turbulence caused by wing vortices absorb - increased induced drag
Induced drag reduced - higher aspect ratio
Lift augmentation devices - increase lift at slow speed (takeoff landing)
Wing fences used to reduce - effects of span-wise flow
Directional stability - sweepback of wing and vertical tail
Control surfaces give longitudinal control - elevators
Acceleration - change of velocity divided by time during which change occurs
Resistance of skin friction of air passes - parasite drag
Lift produced by an airfoil is resultant - relative wind
Types of stability - dynamic and static
Generally center of pressure
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