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 35
N.A.C.A. Technical Kote Ko. 458 Jig. 8 … 00 10° 20° 30° 400 500 gOO Difference in angle of ailerons, 6 Figure 8. Variation of rolling moment coefficient with aileron deflection for the multiple tip ailerons, a = 10°
NASA Technical Reports Server (NTRS)
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