Method for determining load factors in high-angle-of-attack condition by use of two rational variables and one empirical coefficient applied to some 19 airplanes; results compared with factors established by current practice; coordination of wing and tail-loading conditions by establishing limiting velocities for various maneuvers. (See also - discussion p 39-44; Aircraft Eng. v 4 n 36 Feb 1932 p 45-9)
Rationalization of load factors for airplanes in flight
Soc Automotive Engrs J
Society of Automotive Engineers -- Journal ; 30 , n 1
1932
9 pages
Article (Journal)
English
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