Stress distribution within aircraft structure due to temperature gradients and their influence on strength and stiffness.


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    Title :

    Thermo-elastic formulae for analysis of beams


    Additional title:

    Aircraft Eng


    Contributors:
    Hemp, W.S. (author)

    Published in:

    Publication date :

    1956


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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