Development of a Non-autorotative Airplane Capable of Steep Landing (1931)
NASA Technical Reports Server (NTRS) · leaf 33
Figs.12,13 N.A.C.A. Technical Memorandum lTo.650 a,Monoplane wing of Fig. 7 d.Low wing type monoplane,Junkers A35 … Fig.12 Lift coefficient plotted against drag coefficient. a = 0" r 2 Pig. 13 Lift distribution over span of monoplane wi&g of Pig. 7
NASA Technical Reports Server (NTRS)
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