Analysis of 2-spar cantilever wings with special reference to torsion and load transference (1936)
NASA Technical Reports Server (NTRS) · leaf 2
ximate numerical integration or perhaps a by a rib at the tip. For convenience, the cross sections graphical one. are at first assumed constant. Estimate of torsional stiffness required.—Formula The load is a torque, exerted by equal and opposite (6) shows that the relief moment depends on the… … Fioote 6.—Diagram for analysis of wing frame with one rib. the second condition of continuity. The relative vertical displacement at the cut due to spacing may be considered as fixed by other design the external forces is considerations, it is evident that an increase of relief action can be…
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