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The model for the calculation of the thermal strain coeffitient of the compaund oriented composites with given fiber orientation is presented. The mutual sliping of layers are strained by the elastic law. The relations for the calculations of the axial and angular thermal strain coefficient depending on the thermal and elastic pro— perties of each layer are obtained and verified for carbonplastic specimens.
Areg M. Simonian
"Thermodimensional stable structure of composites", Proc. SPIE 2443, Smart Structures and Materials 1995: Smart Structures and Integrated Systems, (8 May 1995); https://doi.org/10.1117/12.208327
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Areg M. Simonian, "Thermodimensional stable structure of composites," Proc. SPIE 2443, Smart Structures and Materials 1995: Smart Structures and Integrated Systems, (8 May 1995); https://doi.org/10.1117/12.208327