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Approximate calculation of multispar cantilever and semicantilever wings with parallel ribs under direct and indirect loading (1932)

NASA Technical Reports Server (NTRS) · leaf 15

An illustration from Approximate calculation of multispar cantilever and semicantilever wings with parallel ribs under direct and indirect loading, 1932, leaf 15 — -J = CD <_ag-> < k(i) k(i) k(i) (1) 4 11-2 n-1 « Fig, 2 Determination of elastic axis of wing. to

NASA Technical Reports Server (NTRS)

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