Investigation of supersonic aircraft configurations composed of cambered body positioned certain distance beneath arbitrary lifting wing; expressions for drag and lift are obtained from reverse flow considerations; variational problem of determining optimum wing incidence and body shape, for given volume and length, to yield minimum drag for prescribed lift; results of numerical calculations for 3 configurations with rectangular wing and one with triangular wing having supersonic leading edges.


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    Titel :

    Body under lifting wing


    Weitere Titelangaben:

    J Aerospace Sciences


    Beteiligte:
    Chen, C.F. (Autor:in) / Clarke, J.H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1961


    Format / Umfang :

    16 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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