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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    Titel :

    Calculation of Supersonic Aerodynamic Influence Matrices


    Untertitel :

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


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    01.01.1961


    Format / Umfang :

    4 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch






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