Wind tunnel research comparing lateral control devices, particularly at high angles of attack XI : various floating tip ailerons on both rectangular and tapered wings (1933)
NASA Technical Reports Server (NTRS) · leaf 34
U.A.C.A. Technical Note JIo. 458 Jig. 7 … 500 100 200 300 400 00 Difference in angle of ailerons, 6 Figure 7. Variation of rolling moment coefficient with. aileron_ deflection for -Qie narrow-chord tip ailerons, a = 10°
NASA Technical Reports Server (NTRS)
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