There are three lateral dynamic attitudes, delineated by rolling, yawing, and sideslipping. It is possible to solve for the pressures on the rolling wing by quasi-steady analysis. This approach is, however, inapplicable for the yawing or sideslipping wing, and it is with the latter two cases that this paper deals.


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    Title :

    Institute of the Aeronautical Sciences Annual Meeting


    Subtitle :

    Summaries of Papers Presented to the 23rd Annual General Meeting Held in New York on January 24–27, 1955


    Published in:

    Publication date :

    1955-04-01


    Size :

    8 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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