Unformatted text preview: l , α L =0, c m,L.E. , and the moment about the aerodynamic center (c/4), c m,A.C. . Question 2: An airplane is designed for a take-off speed of 50 m/s with a maximum coefficient of lift equal to 1.2. What is the maximum wing loading in both SI and English units? 1...
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- Spring '11
- Aerodynamics, Maximum wing loading, Flight Mechanics Homework