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Volumn 26, Issue 9, 2004, Pages 983-992

Fatigue crack propagation for a through thickness crack: A crack propagation law considering cyclic plasticity near the crack tip

Author keywords

KRPG; Cyclic plasticity; Fatigue crack closure model; RPG (re tensile plastic zone generated) load; Threshold of stress intensity factor range

Indexed keywords

CHEMICAL ANALYSIS; CYCLIC LOADS; FATIGUE OF MATERIALS; PLASTIC DEFORMATION; PLASTICITY; RESIDUAL STRESSES; STRESS INTENSITY FACTORS; SURFACE TREATMENT;

EID: 2942708221     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ijfatigue.2003.12.006     Document Type: Article
Times cited : (92)

References (15)
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  • 4
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    • [in Japanese]
    • Toyosada M., Yamaguchi K., Niwa T., Takenaka H., Kajimoto K., Yajima H. Proposal of new parameter for fatigue crack propagation rate based upon the compliance changing phenomena and the development of its measuring method. Journal of Society of Naval Architects of Japan. 169:1991;245-255. [in Japanese].
    • (1991) Journal of Society of Naval Architects of Japan , vol.169 , pp. 245-255
    • Toyosada, M.1    Yamaguchi, K.2    Niwa, T.3    Takenaka, H.4    Kajimoto, K.5    Yajima, H.6
  • 6
    • 0028669672 scopus 로고
    • The significance of RPG load for fatigue crack propagation and the development of a compliance measuring system
    • Toyosada M., Niwa T. The significance of RPG load for fatigue crack propagation and the development of a compliance measuring system. International Journal of Fracture. 67:1994;217-230.
    • (1994) International Journal of Fracture , vol.67 , pp. 217-230
    • Toyosada, M.1    Niwa, T.2
  • 8
    • 0019627111 scopus 로고
    • A crack-closure model for predicting fatigue crack growth under aircraft spectrum loading
    • Newman Jr JC. A crack-closure model for predicting fatigue crack growth under aircraft spectrum loading. NASA Technical Memorandum 81941, 1981.
    • (1981) NASA Technical Memorandum 81941
    • Newman Jr., J.C.1
  • 10
    • 0003490132 scopus 로고
    • FASTRAN-II: A fatigue crack growth structural analysis program
    • Newman Jr JC. FASTRAN-II: a fatigue crack growth structural analysis program, NASA Technical Memorandum 104156, 1992.
    • (1992) NASA Technical Memorandum 104156
    • Newman Jr., J.C.1
  • 11
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    • A study on plastic shrinkage coefficient of crack opening/closing model at a crack extension
    • [in Japanese]
    • Niwa T., Toyosada M. A study on plastic shrinkage coefficient of crack opening/closing model at a crack extension. Journal of Society of Naval Architects of Japan. 188:2000;669-678. [in Japanese].
    • (2000) Journal of Society of Naval Architects of Japan , vol.188 , pp. 669-678
    • Niwa, T.1    Toyosada, M.2
  • 14
    • 2942740728 scopus 로고
    • A study on elasto-plastic behavior and fracture characteristics of notched plate tensile specimen
    • [in Japanese]
    • Yada T., Sakai K., Iino N., Sakano K. A study on elasto-plastic behavior and fracture characteristics of notched plate tensile specimen. Journal of Society of Naval Architects of Japan. 145:1973;425-435. [in Japanese].
    • (1973) Journal of Society of Naval Architects of Japan , vol.145 , pp. 425-435
    • Yada, T.1    Sakai, K.2    Iino, N.3    Sakano, K.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.