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Unformatted text preview: m = - h Hint: Use an approach identical to the worked-out example 4.2 in the text. 3. Consider a symmetric airfoil, with a flap hinged at x= x f . This flap is deflected by an angle so that the camber line looks like the sketch below. Show that the lift generated by the flap deflection is given by: ( 29 [ ] ( 29 ( 29 cos 1 2 1 : such that defined is where 1 cos sin 2 1 2 2 4 / ,-=-= +-= f c m l x C in C Hint: Use an approach similar to problem #2 above....
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This note was uploaded on 10/23/2011 for the course AE 3003 taught by Professor Yeung during the Fall '08 term at Georgia Institute of Technology.
- Fall '08