Journal Published Online: 01 December 1993
Volume 15, Issue 4

Stress-Strain Analysis of a [0/90] Titanium Matrix Laminate Subjected to a Generic Hypersonic Flight Profile

CODEN: JCTRER

Abstract

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Author Information

Johnson, WS
NASA Langley Research Center, Hampton, VA
Mirdamadi, M
NASA Langley Research Center, Hampton, VA
Bahei-El-Din, YA
Cairo University, Gaiza, Egypt
Pages: 7
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Stock #: CTR10382J
ISSN: 0884-6804
DOI: 10.1520/CTR10382J