Development of the Rules Governing the Strength of Airplanes. Part I : German Loading Conditions up to 1926 (1933)
NASA Technical Reports Server (NTRS) · leaf 63
Figs. 16,17,23 IT.A.C.A. Technical Memora.nd\i:,i Ho."^16 … 1916, page 8). -5 0 i 5 10 ^O" 20 •3.8 2.5 It C 412.000 0 t Case C e, 1220 •' •D Case 3 ■ in, 1000 B 990 n, A +2.000 700 r, -0.970 f-=~/^'^^----=Z'T D 650 s, Co.se D 4^ t /; 4E5 u, V -5.320 , D 230 V, -7.584 -y B 225 w, d '-a 110 Figure 16.-Distribution of total air- plane weight A over the spars…
NASA Technical Reports Server (NTRS)
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