This paper describes a routine for calculating supersonic aerodynamic influence matrices, which is suitable for the digital computer. The method is first applied to a wing with straight leading edges, streamwise tips and a supersonic trailing edge. Then, an extension is given which enables wings of arbitrary planform (including those with subsonic trailing edges) to be treated without revision of the original programme.


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    Title :

    Calculation of Supersonic Aerodynamic Influence Matrices


    Subtitle :

    A Numerical Method for Wings of Arbitrary Planform Suitable for Solution on the Digital Computer


    Contributors:


    Publication date :

    1961-01-01


    Size :

    4 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English







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