The dangerous flat spin and the factors affecting it (1931)
NASA Technical Reports Server (NTRS) · leaf 43
N.A.C.Ai Technical Memorandum No,629 Figs.8,9 Fig.8 For calculating the cross-wind force. … 30° 40° 60° 80° a Fig.9 Coefficients of wing lift and drag plotted against angle of attack with parameter
NASA Technical Reports Server (NTRS)
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