Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 124
onstruction condition of loading are the determining factors of the problem, andthat the factor of spar stiffness does not affect the distribution under thisassumption. In justification of this method of distribution of loadbetween the spars the example in Fig. 63 is shown. Here a standardtwo-spar… … Fig. 61 -to*/ond*e 10 \ /7* /3 /4 \ * 3 \\° 1 V 1 lii* M m\ 9 1 liil *e* . O ^ zo >M e •1 p7* /<3 Computet/on3 of £>fx?ct/oa/s /ox ax re tyixjxjj =.sssw+.oz7W=jaeiv 7ZXdi$sX4+^X3x-f^*£ZZW-i-,os6 W*.E76 W J39WFig. 62 J 5X£X]fe 105 Wing Stress Analysis Art. 82 . /9./0 S4 2V /6 t2- - /0~ 30 1…
Airplanes
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