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Structural analysis and design of airplanes (1920)

United States. Army. Air Corps · [Washington] · leaf 266

An illustration from Structural analysis and design of airplanes, 1920, leaf 266
246 Art. 164 Summary of Stresses in Fuselage … Fig. 167. Stress Diagram for Front Portion of Fuselage in Three Point Landing Condition 247 oo < oooo O 00 fel 00 c< 00 .9 CO &J0 <u £ (=1i—I OS Eu+J VO C<l Tt rH (\] O N l> rn C^ MD N Tf rH (NJ O t^ IN l^ ^ rH|S^ 00T^iLOOOCNONMCOiom^)000N-iMW CM OO t^ CM CM -■—i i—…

Airplanes

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