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Relative Economy of Different Methods of Airplane Construction (1931)
NASA Technical Reports Server (NTRS) · leaf 51
Fig.10 N.A.CA. Technical Memorandum No.618 … 5270 bf True length=. c,True length- 2 680 1935 -7700 ^ * k-1480-*H d,630 * f, 610 Applies to 280 ji-^T g. ,525 lower wing also. i.True lengths: 895 j ,Truc lengths: 1315NASA Technical Reports Server (NTRS)
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