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Theoretical span loading and moments of tapered wings produced by aileron deflection (1937)
NASA Technical Reports Server (NTRS) · leaf 31
0 A .6 .8 1.0 Raf/o of Hp chord to roof chord, A Tlgurt 8.- Yaxt&tion of % with aapoot patio and tspor.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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