Effect of Variation of Chord and Span of Ailerons on Rolling and Yawing Moments at Several Angles of Pitch (1931)
NASA Technical Reports Server (NTRS) · leaf 8
EFFECT OF VARIATION OF CHORD AND SPAN OF AILERONS 14 … FKii'HK l.-).-r. S. A. 27 wing section. Ci. and (\v for up aileronangles Figuke IO.-U. S. A. 27 wing section. Cl and Cs for down aileron versus per cent aileron chord of wing chord. Pitch angle, 8°. Span, angles versus per cent aileron chord of wing chord. Pitch angle, 8°. 20 inches (67 per cent of…
NASA Technical Reports Server (NTRS)
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