Reference to previous drag studies involving superimposed or " combined" flow field; method for determining mathematically combined disturbances field, and in certain cases minimum drag, of wings at supersonic speeds; example is provided by wing of elliptic plan form, which achieves minimum drag when lift is distributed uniformly over surface.


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    Titel :

    Theoretical determination of minimum drag of airfoils at supersonic speeds


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:
    Jones, R.T. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1952


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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    Optimal bodies for minimum total drag at supersonic speeds

    MOGA, N. / DEJARNETTE, F. | AIAA | 1981


    Supersonic channel-airfoils for reduced drag

    Ruffin, Stephen / Gupta, Anurag | AIAA | 1997