BEFORE a detailed consideration of internal stresses may be made, it is necessary to define external loadings which are possibly critical. This involves the consideration of manoeuvres throughout the altitude range of the aeroplane, to a severity fixed by aerodynamic or specification values of speed and normal acceleration.


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    Title :

    Practical Structural Design Problems of Supersonic Aircraft


    Contributors:
    Heath, W.G. (author) / Heath, B.O. (author)

    Published in:

    Publication date :

    1957-07-01


    Size :

    10 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    Practical structural design problems of supersonic aircraft

    Heath, W.G. / Heath, B.O. | Engineering Index Backfile | 1957


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    Michell, F.P. | Engineering Index Backfile | 1956


    Structural problems of supersonic aircraft

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    Hunn, B.A. | Engineering Index Backfile | 1953


    SUPERSONIC AND TRANSONIC AIRCRAFT PROBLEMS

    REICHERT, CARL E. | SAE Technical Papers | 1950