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)


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    Title :

    Rationalization of load factors for airplanes in flight


    Additional title:

    Aircraft Eng


    Contributors:

    Published in:

    Publication date :

    1932


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Rationalization of load factors for airplanes in flight

    Newell, J.S. | Engineering Index Backfile | 1932


    The Rationalization of Load Factors for Airplanes in Flight

    Newell, Joseph S. | SAE Technical Papers | 1932


    Load factors on airplanes

    Engineering Index Backfile | 1932


    Rationalization of load factors for aeroplane wings

    Crossland, C.W. | Engineering Index Backfile | 1934


    Flight tests on airplanes

    Koppe, H. | Engineering Index Backfile | 1926