Desirability of expanding airplane regulations to include proof of safety for unsymmetrical loading, at least in structural members specially stressed; flight cases involve increases of customary load assumptions through yawing and rolling moments; corresponding increases in their magnitude can be found; stresses particularly great in case of one-sided landing shock, because principal part of total inertia of plane lies in wings. From Zeit. fuer Flugtechnik und Motorluftschiffahrt, June 14, 1929.
Unsymmetrical forces in an airplane cell
Nat. Advisory Committee Aeronautics -- Tech. Memo
1929
9 pages
4 Figs.
Report
English
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