Load assumptions for calculating the strength of airplanes (1930)
NASA Technical Reports Server (NTRS) · leaf 33
N.A.C.I. Technical Memorandum No. 581 Specification No. 9136 … IIa:P*0.35 eO IIh:P«0.5 eO IIc:P=0.2 eG Position of re- sultants as in la, It u Ic. Ila-c Plight direction-* Landing P'0.12 eO on one P=0.4 eO (overlapping only with Ha) float Ic Stern landing Ilia Side landing (how) At I, P*0.25 eG (overlapping only with lib) P=O.Qg eO (overlapping only with lie)…
NASA Technical Reports Server (NTRS)
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