The dangerous flat spin and the factors affecting it (1931)
NASA Technical Reports Server (NTRS) · leaf 44
N.A.C.A. Technical Memorandum No.G29 Figs.10,11,13 … Fig.10 Coefficients of airplane lift and drag plotted against angle of attack with parameter bnx/2v (n]_ instead of n2) • .6 % *2 20° 40° 60° 80° a Fig.11 Coefficients of aerodynamic moments about spar axis plotted against angle of attack. Fig.13 Coefficients of normal and tangential forces of wing…
NASA Technical Reports Server (NTRS)
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