SCOPUS 정보 검색 플랫폼

Volumn 47, Issue 1-4, 1999, Pages 483-490

An engineering approach for predicting residual strength of carbon/ epoxy laminates after impact and hygrothermal cycling

(2) Qi, B a Herszberg, I b

a Cooperative Research Centre for Advanced Composite Structure Ltd ^* (Australia)

b RMIT UNIVERSITY (Australia)

Author keywords

Carbon epoxy composites; Compression after impact; Hygrothermal; Residual compressive strength

Indexed keywords

CARBON; COMPRESSIVE STRENGTH; EPOXY RESINS; FAILURE (MECHANICAL); STIFFNESS; STRESS CONCENTRATION; THERMAL CYCLING;

CARBON EPOXY LAMINATES; COMPRESSION AFTER IMPACT; HYGROTHERMAL CYCLING; IMPACT DAMAGE; PLAIN WOVEN FABRIC LAMINATES; POINT STRESS FAILURE; RESIDUAL COMPRESSIVE STRENGTH; RESIN TRANSFER MOULDING;

LAMINATED COMPOSITES;

ANALYSIS; COMPRESSIVE PROPERTY; DAMAGE; FIBER REINFORCED COMPOSITE; STRESS; WOVEN FABRIC;

EID: 0033304463 PISSN: 02638223 EISSN: None Source Type: Journal
DOI: 10.1016/S0263-8223(00)00027-1 Document Type: Conference Paper

Times cited : (39)

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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.