Notes on the calculation of the minimum horizontal tail surface for airplanes equipped with wing flaps (1937)
NASA Technical Reports Server (NTRS) · leaf 24
N.A.O.A. Technical Note Wo 597 Pig. 5 … -.2 -.1 0 .1 .B Hinge-moment coefficient Figure 5.- Uffect of ratio of elevator chor.d to total tail- surf SLce chord on h-unge-moment coefficient, (reference 6); aspect ratio, 4.3
NASA Technical Reports Server (NTRS)
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