Basis for expectation that economic long range aviation is about to be transformed; design barrier and structure weight penalties; existence of two different values of lift/drag ratio for same aircraft announces that ideal shape for subsonic flight is different from ideal shape for supersonic flight; aerodynamic necessity for variable shape inexorably exists.


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    Title :

    Supersonic turning-point


    Additional title:

    Shell Aviation News


    Contributors:
    Goddard, V. (author)

    Published in:

    Publication date :

    1959


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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