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 12
nt aileron chord of wing chord Figure 34.—Clark Y wing section. 'NIL for combined ailerons (right Figure 33.—Clark Y wing section. for combined ailerons (right up, left down) versus per cent aileron span of wing semispan. Pitch up, left down) versus per cent aileron chord of wing chord. Pitch… … Per cenf o He ran chord of wing chord Per cenf aileron chord of wing chord Figure 36.—U. S. A. 27 wing section. Ci and Cn for down aileron angles Figure 35.—U. S. A. 27 wing section. Cl and Cn for up aileron angles versus per cent aileron chord of wing chord. Pitch angle, 12°. Span, versus per cent…
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
