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Old 23rd Jul 2016, 12:00
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issaccph
 
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Question about zero lift angle of attack
Hi,

For an average cambered wing like that found on a typical training aircraft, such as a Cessna 172, at about -4 angle of attack, the lift is zero and CL = 0.

But is it possible to achieve -4 angle of attack on a Cessna 172? If so, how to do it?

Thanks,
Issac
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