The Pressure Distribution Over the Horizontal Tail Surfaces of an Airplane I (1923)
NASA Technical Reports Server (NTRS) · leaf 26
CASE T. 600 R.P.M. CASE H. 600 R.P.M. CASE HT. 600 R.P.M. CASE Y. 600 ft. P.M. CASE W. 600 R.P.M. C.G. Coefficient '.38/ C.G. Coefficient =.326 CG. Coefficient = 326 C.G. Coefficient =.244 CG. Coefficient-.370 … VARtATtO/V OF PRESSURE WITH A/ft SPEED. Positive pressure is p/otted upward fjg 34 from the chord os o hose line.
NASA Technical Reports Server (NTRS)
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