Effect of aspect ratio on lift curve and on maximum resultant force coefficient; effect of tip shape on profile drag and angle of attack for infinite aspect ratio.


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    Title :

    Some considerations regarding airfoils of extremely low aspect ratio


    Additional title:

    Aeronautical Sciences -- J


    Contributors:

    Published in:

    Publication date :

    1935


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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