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Structural analysis and design of airplanes (1920)

United States. Army. Air Corps · [Washington] · leaf 293

An illustration from Structural analysis and design of airplanes, 1920, leaf 293
q. in. for Fig. 176= mnpq3h lbs. per in.2. For Fig. 177, let 1 in. = r sq. in. from Fig. 176. Then 1 in. in Fig.177 = rmnpq3h lbs. per in.1. If the pole distance for Fig. 177 is hx in.the scale of ordinates for the deflection polygon is 1 in. = rmnpq4hh1 lbs.per in. The value of the ordinates…

Airplanes

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