THE highly complex character of the gust-load problem and the lack of knowledge of gust structure have led to the general use of gust-strength criteria for aeroplane wings that are based on the concept of a “sharp-edged” gust in which the aerodynamic phenomena are assumed to obey the laws of steady flow.


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    Title :

    The Gust-Load Problem


    Subtitle :

    The Results of Acceleration Data Obtained on Large and Small Commercial Aeroplanes in America


    Contributors:

    Published in:

    Publication date :

    1937-08-01


    Size :

    6 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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