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Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 111
/29^ \<?6> Struts of St a. ®5P/9/2 &£#CT/0/VS FO& COMPUT/NO D&/FT Fig. 52 … soz- »L 3 .?* ^pj_ v55^ Chord Fig. 53. Wire in Outer and Center Section 92 Art. 72 Drag Components of Struts and Wires TABLE IXa WireG Length89.3 in. Drag9.25 89.3 Comp.= —.104 Stress/Vert. Comp.89.3 =1.654 54.0 B 96.0 in. 36.696.0 - -.382 96.0 =1.779 54.0 C 97.9 in. 38.497.9 = +.392 97.9 =1.749…Airplanes
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