Lowspeed stall will start at the wings trailing edge a. where C1/CL is a minimum. b. Where
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Low‐speed stall will start at the wing’s trailing edge
a. where C1/CL is a minimum.
b. Where C1/CL is a maximum.
c. at the root for a swept wing.
d. at the wingtip for a straight rectangular wing.
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Related Book For
Flight Theory And Aerodynamics
ISBN: 9781119772415
4th Edition
Authors: Joseph R. Badick; Brian A. Johnson
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