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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    Titel :

    Resistance of Delta wing in supersonic flow


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Memo


    Beteiligte:
    Karpovich, E.A. (Autor:in) / Frankl, F.I. (Autor:in)


    Erscheinungsdatum :

    1951


    Format / Umfang :

    6 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Resistance of a delta wing in a supersonic flow

    Karpovich, E. A. / Frankl, F. I. | TIBKAT | 1951


    Resistance of a delta wing in a supersonic flow

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


    Delta-wing configurations for supersonic transport

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


    Supersonic vortex breakdown over a delta wing in transonic flow

    KANDIL, HAMDY / KANDIL, OSAMA / LIU, C. | AIAA | 1993


    Supersonic Vortex Breakdown over a Delta Wing in Transonic Flow

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