Download Thermal Residual Stresses in Silicon-Carbide/Titanium (0/90) Laminate - National Aeronautics and Space Administration file in PDF Online

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The current work formulated a micromechanical analysis of a cross-ply laminate and calculated the thermal residual stress in a very thick (0/90)(sub 2n) silicon-carbide/titanium laminate. Results were also shown for a unidirectional laminate of the same material. Discrete fiber-matrix models assuming a rectangular array of fibers with a fiber volume fraction of 32.5

Title : Thermal Residual Stresses in Silicon-Carbide/Titanium (0/90) Laminate
Author : National Aeronautics and Space Administration
Language : en
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Type : PDF, ePub, Kindle
Uploaded : Apr 03, 2021

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