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    Title :

    Effect of streamline contouring in the wing-fuselage juncture in combination with the supersonic area rule on a sweptback-wing-fuselage configuration of high fineness ratio


    Contributors:

    Published in:

    D ; 387


    Publication date :

    1960


    Size :

    19 S


    Remarks:

    Ill., graph. Darst


    Type of media :

    Book


    Type of material :

    Print


    Language :

    English





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    KUBENDRAN, L. / MCMAHON, H. / HUBBARTT, J. | AIAA | 1985


    Turbulent flow around a wing/fuselage-type juncture

    Kubendran, L. R. / Mcmahon, H. M. / Hubbartt, J. E. | NTRS | 1986


    Flow control in a wing/fuselage-type juncture

    KUBENDRAN, L. / BAR-SEVER, A. / HARVEY, W. | AIAA | 1988