Cantilever Wings for Modern Aircraft: Some Aspects of Cantilever Wing Construction with Special Reference to Weight and Torsional Stiffness (1929)
NASA Technical Reports Server (NTRS) · leaf 17
G.A. Technical Le no randua No.5 58 SlgB-4 I 5 Seni-span ■ 35.5 f t … II III IV Bulkheads a, Drag and torsion wires b, Compression tubes and fittings. c, Wiring fittings. d, Bulkheads. Fig.4 Weight distribution of various components along the spar. A p a, Actual •H • lO b, Ideal 8 rj ,Q 4 P.r-1 40 0 10 20 30 Distance in feet Fig.5 Comparison between actual and ideal…
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