Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 149
££/?& C/93/PA/6 System 5/oe £l£i//?T/OM £6+\*l-^/&.9-4 … NOTE: LENGTHS 0/l/£A/ OH n£M3E£3 /?&£ aCTCS/ll. L£MGTH>5. Fig. 86. Tripod System of Center Section Struts 130 Art. 100 Center Section Struts The conditions of equilibrium are applied to the components of allthe forces and loads applied at a point and resolved along three axes atright angles.…
Airplanes
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