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.
Thermal Stresses in I-section Beams
Stress Distributions Due to Arbitrary Temperature Distributions for I-section Beams or Multicell-section Beams Built Up from I-section Units
Aircraft Engineering and Aerospace Technology ; 34 , 11 ; 320-324
1962-11-01
5 pages
Article (Journal)
Electronic Resource
English
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