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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Flight Theory And Aerodynamics

ISBN: 9781119772415

4th Edition

Authors: Joseph R. Badick; Brian A. Johnson

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