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Volumn 50, Issue 10, 2011, Pages 2793-2813

XFEM fracture analysis of shells: The effect of crack tip enrichments

Author keywords

Crack tip enrichment; Crack tip opening angle (CTOA); Extended finite element method (XFEM); Shells

Indexed keywords

BENCHMARK TESTS; CRACK TIP OPENING ANGLE; CRACK TIP OPENING ANGLE (CTOA); CRACK TIP OPENING DISPLACEMENT; EXTENDED FINITE ELEMENT METHOD; EXTENDED FINITE ELEMENTS; FRACTURE ANALYSIS; FRACTURE MECHANICS PARAMETERS; FRACTURE MODE; HIGH ORDER; IN-PLANE; OUT-OF-PLANE; ROTATIONAL DEGREES OF FREEDOM; SHELLS;

EID: 79959495553     PISSN: 09270256     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.commatsci.2011.04.034     Document Type: Article
Times cited : (63)

References (67)
  • 62
    • 0005768590 scopus 로고
    • Axial Crack Propagation and Arrest in Pressurized Fuselage
    • M. Kosai, and S. Kobayashi Axial Crack Propagation and Arrest in Pressurized Fuselage S.N. Atluri, S. G Sampath, P. Tong, Structural Integrity of Aging Airplanes 1991 Springer-Verlag Berlin, Germany 225 239
    • (1991) Structural Integrity of Aging Airplanes , pp. 225-239
    • Kosai, M.1    Kobayashi, S.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.