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 18
^ 0 5 10 15 20 Distance from und of test section,feet. Note Structure e'esignud to a factor of 3.25 W.Test section tapered in pl,an form and a thickness/ chord ratio of 0.18 used throughout. Fig.6 Torsional deflection for 1 S. loading and ± I0/o CP. movement. Note 1.20 Limitation of deflection… … stiff triangle due to aileron, Fig.8
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