Developments in high speed aircraft and missiles have resulted in trend toward using thin airfoils of short span, making it necessary to obtain reasonable predictions for aerodynamic load in tip region and at moderate angle of attack; theoretical investigation on simplified model. Bibliography.


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    Title :

    Aerodynamics of rectangular plate with vortex separation in supersonic flow


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Cheng, H.K. (author)


    Publication date :

    1955


    Size :

    10 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English







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