Analytical and experimental tools available to meet demands of high speed flight upon aircraft structures; status with respect to heat transfer from boundary layer into structure, modes of failure under combined load as well as thermal inputs and aerothermoelasticity; methods of alleviating structural and aeroelastic problems of high speed flight. 19th Wright Brothers Lecture. (See also - discussion p 321-9)


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    Title :

    Some structural and aeroelastic considerations of high-speed flight


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1956


    Size :

    33 pages


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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