Download Simplified Micromechanical Equations for Thermal Residual Stress Analysis of Coated Fiber Composites - National Aeronautics and Space Administration file in PDF Online

Full Download Simplified Micromechanical Equations for Thermal Residual Stress Analysis of Coated Fiber Composites - National Aeronautics and Space Administration | ePub

The fabrication of metal matrix composites poses unique problems to the materials engineer. The large thermal expansion coefficient (CTE) mismatch between the fiber and matrix leads to high tensile residual stresses at the fiber/matrix (F/M) interface which could lead to premature matrix cracking during cooldown. Fiber coatings could be used to reduce thermal residual

Title : Simplified Micromechanical Equations for Thermal Residual Stress Analysis of Coated Fiber Composites
Author : National Aeronautics and Space Administration
Language : en
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Type : PDF, ePub, Kindle
Uploaded : Apr 06, 2021

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