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Volumn 34, Issue 9, 1996, Pages 1449-1454

The role of crack closure in fatigue crack propagation behaviour of a TiAl-based alloy

Author keywords

[No Author keywords available]

Indexed keywords

COMPOSITION; CRACK PROPAGATION; FATIGUE OF MATERIALS; INTERMETALLICS; MECHANICAL VARIABLES MEASUREMENT; METALLOGRAPHIC MICROSTRUCTURE;

EID: 0030151856     PISSN: 13596462     EISSN: None     Source Type: Journal    
DOI: 10.1016/1359-6462(95)00679-6     Document Type: Article
Times cited : (13)

References (8)
  • 3
    • 0015055746 scopus 로고
    • ASTM STP 486, Toronto, Ontario, Canada, Ed., American Society for Testing and Materials, Philadelphia, Pa
    • Elber W., Damage Tolerance in Aircraft Structures, ASTM STP 486, Toronto, Ontario, Canada, Vol. ASTM STP 486, Ed., American Society for Testing and Materials, Philadelphia, Pa., 230-242 (1971).
    • (1971) Damage Tolerance in Aircraft Structures , vol.ASTM STP 486 , pp. 230-242
    • Elber, W.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.