Search NASAโŒ• Search

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.

Explore related subjects

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Raj, S. V.. 2016-02-01. Thermal Expansion Behavior of Hot-Pressed Engineered Matrices. https://ntrs.nasa.gov/citations/20160001712

Cite the original work for its findings. Save a collection to share your selection of sources.