Experimental data have shown that decrease in aspect ratio of wing decreases adverse effects of compressibility on wing; approximate method by which quantitative effect of variation of aspect ratio can be predicted.


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    Title :

    Aspect ratio influence at high subsonic speeds


    Additional title:

    J. Aeronautical Sciences


    Contributors:


    Publication date :

    1956


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :