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Load assumptions for calculating the strength of airplanes (1930)

NASA Technical Reports Server (NTRS) · leaf 29

An illustration from Load assumptions for calculating the strength of airplanes, 1930, leaf 29 — N.A,C4» Technical Memorandum No.581 >.9032 «J» €V3 O .03 C3 03 •jtoq.o'Bj pt?ox agrees < u

NASA Technical Reports Server (NTRS)

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