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 6
5 EFFECT OF VARIATION OF CHORD AND SPAN OF AILERONS … 15 20 . 25 30 35 15 20 P5 30 35 Per cent aileron chord of wing chord Per cent aileron chord of wing chord FKiUKE Clark Y wing section. Cl and C.v for down aileron angles KiGURK ').—Clark Y wing section. Cl and C.v for up aileron angles versus per cent aileron chord of wing chord. Pitch angle 8°.…
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