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Effect of aileron displacement on wing characteristics (1933)
NASA Technical Reports Server (NTRS) · leaf 21
Figure 9.-Vector diagram, 20 by 2 inch aileron, ri^it up, left down. 0 = 0. Clark Y airfoil. ■mNASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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