Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 260
brium. The vertical reactions figured at thechassis strut points do not represent functions of the stresses in thechassis struts under the landing condition with the tail up, but are onlythe loads located at the points shown, which will maintain the structurein equilibrium. The stresses shown in… … 241 Fuselage Art. 162 Ik \J * S \f-*M* i ^z^?^! ^ \ ^ \-o ?, -V\ * \ V \ ^ „ \ //~ . f° \ ^ Ov Nf o\ % ^\ r s?- <0 \ / < 1 V k \ / N P y> s- ^> ^ / o1? p/ \ /x r $ 66- $ * 1 * is / N^ <6 Nj ») V QfS- / *0 ^ ft V 1 NjQ / k * 06h- •> f^ <V .Vv 09P- - /* A 0 % X&pel \i 00^^/…
Airplanes
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