Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 292
F/o, 175 Bend/no Moment Equ/l3/?/umPolygon 272 Art 173 Determining Deflection of Beams with Varying Load and Section … Ho. i uroecc Pol yoo/vroe Load/ne Cuei/r Fie. 173, whence 1 in. in For Fig. 173, 1 sq. in. = p X q lbs. For Fig. 174, let 1 in. = n sq. in. fiFig. 174 = n X p X q lbs. If the pole distance for Fig. 174 is h in., the scale for the bendingmoment polygon is 1 in. = n X P X q2 X h in. lbs. If the…
Airplanes
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