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Volumn 80, Issue 2, 1989, Pages 193-218

Application of a closure model to predict crack growth in three engine disc materials

Author keywords

[No Author keywords available]

Indexed keywords


EID: 0005185180     PISSN: 03769429     EISSN: 15732673     Source Type: Journal    
DOI: 10.1007/BF00012669     Document Type: Article
Times cited : (20)

References (17)
  • 1
    • 84950405000 scopus 로고    scopus 로고
    • M.D. Raizenne, AGARD SMP Sub-Committee 33 Engine Disc Test Programme Fatigue Crack Growth Rate Data and Modelling Cases for Ti-6A1–4V, IMI-685 and Ti-17, National Research Council of Canada, Institute of Aerospace Research, LTR-ST-1785, Nov. 1990.
  • 2
    • 84950405001 scopus 로고    scopus 로고
    • A.J.A. Mom and M.D. Raizenne, AGARD Engine Disc Cooperative Test Programme, AGARD Report No. 766, 1988 and AGARD Report No. 766 (Addendum), April 1993.
  • 3
    • 84950405002 scopus 로고    scopus 로고
    • FASTRAN — Fatigue Crack Growth Analysis of Structures — A Closure Model, Computer Software Management and Information Center, University of Georgia, Athens, Georgia, December 1984.
  • 4
    • 84950405003 scopus 로고    scopus 로고
    • J.C. Newman, Jr., A crack-closure model for predicting fatigue crack growth under aircraft spectrum loading, Methods and Models for Predicting Fatigue Crack Growth under Random Loading, ASTM STP 748 (1981) 53–84.
  • 5
    • 84950405004 scopus 로고    scopus 로고
    • J.C. Newman, Jr., Prediction of fatigue crack growth under variable amplitude and spectrum loading using a closure model, Design of Fatigue and Fracture Resistant Structures, ASTM STP 761 (1982) 255–277.
  • 7
    • 84950405005 scopus 로고    scopus 로고
    • A.A. ten Have, Cold Turbistan — Final Definition of a Standardized Fatigue Test Loading Sequence for Tactical Aircraft Cold Section Engine Disc, Nationaal Lucht-en Ruimtevaartlaboratorium, NLR TR 87054 L (1987).
  • 8
    • 84950405006 scopus 로고    scopus 로고
    • W. Elber, The significance of fatigue crack closure, damage tolerance in aircraft structures, in ASTM STP 486 (1971) 230–242.
  • 10
    • 84950405007 scopus 로고    scopus 로고
    • G.R. Irwin, Plastic zone near a crack and fracture toughness, Proceedings of the 7th Sagmore Conference (1960) IV.63–IV.74.
  • 12
    • 84950405008 scopus 로고    scopus 로고
    • R.G. Forman, V. Shivakumar, J.C. Newman, Jr., S.M. Piotrowski and L.C. Williams, Development of the NASA FLAGRO computer program, Fracture Mechanics: Eighteenth Symposium, ASTM STP 945 (1988) 781–803.
  • 13
    • 84950405009 scopus 로고    scopus 로고
    • J.C. Newman, Jr., Discussion on cyclic crack growth transitional behavior, in Fatigue Crack Propagation, ASTM STP 415 (1967) 380–383.
  • 14
    • 84950405010 scopus 로고    scopus 로고
    • J.C. Newman, Jr., Effects of constraint on crack growth under aircraft spectrum loading, in Fatigue of Aircraft Materials, A. Beukers, T. deJong, J. Sinke, A. Vlot and L.B. Vogelesang (eds.), Delft University Press (1992).
  • 15
    • 84950405011 scopus 로고    scopus 로고
    • J.C. Newman, Jr., M.H. Swain and E.P. Phillips, An assessment of the small-crack effect for 2024-T3 aluminum alloy, in Small Fatigue Cracks, R.O. Ritchie and J. Lankford (eds.), Metallurgical Society of AIME (1986).
  • 16
    • 84950405012 scopus 로고    scopus 로고
    • B.E. Powell and I. Henderson, The Conjoint Action of High and Low Cycle Fatigue, AFWAL-TR-83–4119, November 1983.


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.