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Volumn 58, Issue 1-2, 1997, Pages 107-119

Analytical expressions for crack opening displacements of edge cracked specimens under a segment of uniform crack face pressure

Author keywords

Crack opening displacement; Edge crack; Segment uniform pressure; Weight functions

Indexed keywords

BOUNDARY CONDITIONS; FUNCTIONS; PRESSURE EFFECTS;

EID: 0031224021     PISSN: 00137944     EISSN: None     Source Type: Journal    
DOI: 10.1016/s0013-7944(97)00067-2     Document Type: Article
Times cited : (10)

References (6)
  • 2
    • 0019627111 scopus 로고
    • A crack-closure model for predicting fatigue crack growth under aircraft spectrum loading
    • Newman, J. C., Jr, A crack-closure model for predicting fatigue crack growth under aircraft spectrum loading. ASTM STP, 1981, 748, 53-84.
    • (1981) ASTM STP , vol.748 , pp. 53-84
    • Newman J.C., Jr.1
  • 5
    • 0041621926 scopus 로고
    • Small-crack effects in high-strength aluminum alloys. A CAE/NASA Cooperative Program
    • Selected papers Aviation Industry Press (in Chinese), see also NASA RP1309, 1994
    • Wu, X. R., Newman, J. C., Jr, et al., Small-crack effects in high-strength aluminum alloys. A CAE/NASA Cooperative Program, Selected papers in Scientific and Technical International Cooperation Program, Aviation Industry Press (in Chinese), 1994; see also NASA RP1309, 1994.
    • (1994) Scientific and Technical International Cooperation Program
    • Wu, X.R.1    Newman J.C., Jr.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.