The resistance of a delta wing at small angle of attack in supersonic conical flow with its leading edges within the Mach cone is calculated by a method that separates out the suction force.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Resistance of a delta wing in a supersonic flow


    Contributors:

    Publication date :

    1951-04-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Resistance of Delta wing in supersonic flow

    Karpovich, E.A. / Frankl, F.I. | Engineering Index Backfile | 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