Development of a Non-autorotative Airplane Capable of Steep Landing (1931)
NASA Technical Reports Server (NTRS) · leaf 41
N.A.C.A. Technical Memorandum 1Tb*650 Figs.29,30,31,32 … Numerical integration. a Fig.31 Change in angles of attack 20C of glide and in rate of V. a rotation about the lateral axis due to gradual forward displacement of controls. 10° nz(i/s) z -.2 L-U 1 L. V'V 2 3 4, ~ Time, sec / / h,m • • -~ -10' -^e- ——jcts- r 100 200 400! 300 s,m a, With non*-amt…
NASA Technical Reports Server (NTRS)
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