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 Soc Automotive Engrs J v 30 n 1 Jan 1932 p 31-9 and (discussion) 39-44)
Rationalization of load factors for airplanes in flight
Aircraft Eng
Aircraft Engineering ; 4 , n 36
1932
5 pages
Article (Journal)
English
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