Analysis of 2-spar cantilever wings with special reference to torsion and load transference (1936)
NASA Technical Reports Server (NTRS) · leaf 16
he calculation of the pure Consequently, it was assumed as a first approximation torsional stiffness. Since the materials specifications that the relief action was not affected by the flexibility permit 20 percent excess thickness, the calculated of the center section; however, the calculated… … 0 2 3 5 Fioubb 2L—Twist of Driggs-Dart wing. Tip Station Root A very interesting test on a plywood-covered wing Fioubb 20.—Torque and bending moments In Driggs-Dart wing. is described in reference 15. The wing was tested from the known deflections at the center line and at the under, a distributed…
NASA Technical Reports Server (NTRS)
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