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Unformatted text preview: 0.2c and which is deflected 25 degrees.(ie the rear 0.2c of the camber line is deflected downwards account for the change in chord and recall the chord line connects the LE and TE) When the geometric angle of attack is 4 degrees, what is the section lift coefficient? Where is the center of pressure?...
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This note was uploaded on 05/03/2011 for the course AE 2020 taught by Professor Ruffin during the Spring '07 term at Georgia Institute of Technology.
- Spring '07