NASA NTRS ยท 20160001712
Thermal Expansion Behavior of Hot-Pressed Engineered Matrices
Abstract
Advanced engineered matrix composites (EMCs) require that the coefficient of thermal expansion (CTE) of the engineered matrix (EM) matches those of the fiber reinforcements as closely as possible in order to reduce thermal compatibility strains during heating and cooling of the composites. The present paper proposes a general concept for designing suitable matrices for long fiber reinforced composites using a rule of mixtures (ROM) approach to minimize the global differences in the thermal expansion mismatches between the fibers and the engineered matrix. Proof-of-concept studies were conducted to demonstrate the validity of the concept.
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Raj, S. V.. 2016-02-01. Thermal Expansion Behavior of Hot-Pressed Engineered Matrices. https://ntrs.nasa.gov/citations/20160001712
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