Resistance of delta wing at small angle of attack in supersonic conical flow with its leading edges within Mach cone is calculated by method that separates out suction force. English abstract from Prikladnaya Matematika i Mekhanika n 4 1947 p 495-6.


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    Title :

    Resistance of Delta wing in supersonic flow


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Memo


    Contributors:


    Publication date :

    1951


    Size :

    6 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Resistance of a delta wing in a supersonic flow

    Karpovich, E A / Frankl, F I | NTRS | 1951


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    Jones, Jr., J.L. / Hunton, L.W. / Gregory, T.J. et al. | Engineering Index Backfile | 1963


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    Supersonic Vortex Breakdown over a Delta Wing in Transonic Flow

    Kandil, H. / Kandil, O. / Liu, C. et al. | British Library Conference Proceedings | 1993