In design of high speed aircraft, problem of relating structure loads to prescribed flight envelope leads often to necessity of airframes being considerably stronger than past experience suggests; one aspect of problem considered, namely, influence of elasticity upon aircraft derivatives from which tail loads are computed.


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    Title :

    Aspect of deformation of swept wings in steady supersonic flight


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:
    Hunn, B.A. (author) / Lance, G.N. (author)

    Published in:

    Publication date :

    1954


    Size :

    11 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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