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A Short Method of Calculating Torsional Stresses in an Airplane Fuselage (1924)
NASA Technical Reports Server (NTRS) · leaf 29
Comparison of calculated and experimental vp^'.ucg ot" strepee* … bd,Gq.in.center of bay. Fig^9 Top and bottom vdres of fuselage 1400 , "®'= Galdulate'd,formula VI 4 -^- -fo -= -Srde taivxng-doTfn load— 1200 ExperYnental = u " up " ijD = Average 1000 - = 'Yahm'T^mithod by statics ~ ='Pippard and" Prit chard''"s' . 800 CD 0) S 600 400 200 1000 ) 400 600 800 0…NASA Technical Reports Server (NTRS)
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