Development of the rules governing the strength of airplanes. Part III : loading conditions in France, Italy, Holland, and Russia - aims at standardization (1933)
NASA Technical Reports Server (NTRS) · leaf 53
Jigs. 45,46,47 N.A.C.A. Technical Memorandum :!o. 718 - i- 5 Germany, line 2 to 5 stress categories 10 2-5. CI2TA. line 6 to 8 class special, nor- ,<-. - A""" mal and acrobatic. X. England, line 9 to 10 j- 15! \ normal and acrobatic. U.S.A. line 11 to 13 — power loading 9, 6 K 8- o … Gross weight, G 400 1 3.80 g, 1.30 ! a, b, 3.23 h, 0.84 _ t- 300 c, 2.35 i, 0.80 d, 2.30 ... O! h j, 0.63 •+•■- 200 e, 1.75 k, 0.57 •d lO i.'i f, 1.60 1, 0.45 ^ABi J m, 0.54 100 ; Material wd mab- Figure 46.-Wing fail 1 acc: dent • Uf£ turm 3 accadents tires. 100 150 200 250 300 kg/m' Dynaihic…
NASA Technical Reports Server (NTRS)
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