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Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 190
_l_ .. S&K* §8825 rcwS 388££ KS&5 VW» - Vv ^t 1? ^S^sf^^^^^S^^^Ss^si^y (h { II III ~ ~ ----- L. X -U .li-l S 4^^^^rs^^^^^^Q^^,^^ 1 rf HSolooSw^ * A* •* > * * As * « v*vsfsK - -ovxvv r ifi i.. 1111 i«rri i [.til ? ^ q>©<t<5<!>cxI>oc,< v x a5< ££*! ■I,<t<… … Airplane Design Art. 123 load-elongation curve is shown in Fig. 104 is used on the airplane.Below are given the necessary data for the shock absorber. One Unit Length of 4 partial loops = 14.1 in. Length of 1 complete loop = 2(1.67+3.21) = 9.76 in. (See Fig. 105) Number of complete loops = 13 Total…Airplanes
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