Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 261
242 Art. 163 Computation of Loads and Stresses for Three Po:nt Landing Condition of landing with the tail up. If, however, the connections between thefuselage and chassis are made strong enough it is felt that the stressesin the bottom longerons will not become troublesome. There are a num-ber of…
Airplanes
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