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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    Title :

    Body under lifting wing


    Additional title:

    J Aerospace Sciences


    Contributors:
    Chen, C.F. (author) / Clarke, J.H. (author)

    Published in:

    Publication date :

    1961


    Size :

    16 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :





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