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Hi, I'm having a hard time answering this problem for a project . How do the required CL and AOA for the PA-28 at 3,400
Hi, I'm having a hard time answering this problem for a project .
How do the required CL and AOA for the PA-28 at 3,400 lbs change with changes in airspeed?
I understand the relationship between CL & AOA, I just don't know how to give specific examples.
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