Presence of tip reduces lift and performance compared with corresponding values for 2-dimensional wing; it appeared from work by K.STEWARTSON that addition of vane at wing tip might counteract this effect; effect due to presence of vane determined.


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    Title :

    Effect of Delta vanes on supersonic wings


    Additional title:

    Aeronautical Quarterly


    Contributors:

    Published in:

    Publication date :

    1954


    Size :

    29 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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