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Load assumptions for calculating the strength of airplanes (1930)
NASA Technical Reports Server (NTRS) · leaf 32
8pec. Hos. 9121 to 9128 & 9153 N.A.C.A. Tech. Memo. Ho.581 P=eG P=eG P=0.50 eO 9122 Wheel landing 9121 Three-point 912? One-wheel landing landing P P=0.10 eG 9124 Lateral landing shock P=2.0 G P=1.5 0 9125 Nose landing … P-1.5 G 9123 & 9124 Overlapping of individual 9126 Towing loads m. 100$ Specification tfos. 9121 to 9128 & 9153 Load P P=0.15 e8p GSI cases (safe p2=esp asp (91H & 9H2) 9128 Lateral conditions) impact of 9127 Vertical impact skid of skidNASA Technical Reports Server (NTRS)
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