Thermal stresses due to arbitrary temperature distributions are calculated for beams of I-section or of multicell sections which can be considered to be built up from I-section units. Stress distributions are presented graphically for a wide range of the parameters involved. It is shown that for a high-speed aircraft the thermal stresses alone could produce plasticity in a homogeneous structure.


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    Title :

    Thermal Stresses in I-section Beams


    Subtitle :

    Stress Distributions Due to Arbitrary Temperature Distributions for I-section Beams or Multicell-section Beams Built Up from I-section Units


    Contributors:
    Ayers, K.B. (author)

    Published in:

    Publication date :

    1962-11-01


    Size :

    5 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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