메뉴 건너뛰기




Volumn 25, Issue 6, 2005, Pages 11-17

Investigation of small-crack and long-crack propagation behavior in titanium alloy TC4 and aluminum alloy 7475-T7351

Author keywords

Aluminum alloy; Long crack; Small crack; Small crack effect; Titanium alloy

Indexed keywords

AIRCRAFT MATERIALS; ALUMINUM ALLOYS; CRACK INITIATION; CRACK PROPAGATION; INCLUSIONS; TITANIUM ALLOYS;

EID: 30544435486     PISSN: 10055053     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (21)

References (13)
  • 3
    • 85166632633 scopus 로고
    • Fracture mechanics parameter for small fatigue cracks
    • ASTM STP1149
    • NEWMAN J C JR. Fracture mechanics parameter for small fatigue cracks[R]. ASTM STP1149, 1992. 10-33.
    • (1992) , pp. 10-33
    • Newman, Jr.J.C.1
  • 4
    • 0003824593 scopus 로고
    • Small crack effects in high-strength aluminum alloys - A NASA/CAE cooperative program
    • NASA Reference Publication 1309
    • NEWMAN J C JR, WU X R, et al. Small crack effects in high-strength aluminum alloys-a NASA/CAE cooperative program[R]. NASA Reference Publication 1309, 1994.
    • (1994)
    • Newman, Jr.J.C.1    Wu, X.R.2
  • 5
    • 30544439440 scopus 로고    scopus 로고
    • Chinese source
  • 6
    • 0042810316 scopus 로고
    • Small-crack test methods
    • ASTM STP1149
    • LARSEN J M, ALLISON J E. Small-crack test methods [R]. ASTM STP1149, 1992.
    • (1992)
    • Larsen, J.M.1    Allison, J.E.2
  • 7
    • 0003901380 scopus 로고    scopus 로고
    • Standard test method for measurement of fatigue crack growth rates
    • ASTM E647-99
    • Standard test method for measurement of fatigue crack growth rates [R]. ASTM E647-99, 1999. 621-627.
    • (1999) , pp. 621-627
  • 8
    • 0015055746 scopus 로고
    • The significance of crack closure, Damage tolerance in aircraft structures
    • Philadelphia: ASTM STP 486
    • ELBER W. The significance of crack closure, Damage tolerance in aircraft structures [R]. Philadelphia: ASTM STP 486, 1971. 230-242.
    • (1971) , pp. 230-242
    • Elber, W.1
  • 9
    • 0003743642 scopus 로고
    • A crack-closure model for predicting fatigue crack growth under aircraft spectrum loading
    • ASTM STP 748
    • NEWMAN J C JR. A crack-closure model for predicting fatigue crack growth under aircraft spectrum loading [R]. ASTM STP 748, 1986. 427-452
    • (1986) , pp. 427-452
    • Newman, Jr.J.C.1
  • 10
    • 0021405273 scopus 로고
    • A crack-opening stress equation for fatigue crack growth
    • NEWMAN J C JR. A crack-opening stress equation for fatigue crack growth [J]. J of Fracture, 1984, 24: 131-135.
    • (1984) J of Fracture , vol.24 , pp. 131-135
    • Newman, Jr.J.C.1
  • 12
    • 0029531833 scopus 로고
    • Microstructure effects on small fatigue crack initiation and growth in Ti6Al4V alloys
    • DEMULSANT X, MENDES J. Microstructure effects on small fatigue crack initiation and growth in Ti6Al4V alloys [J]. Fatigue Fract Engng Mater Struct, 1995, 18(12): 1483-1497.
    • (1995) Fatigue Fract Engng Mater Struct , vol.18 , Issue.12 , pp. 1483-1497
    • Demulsant, X.1    Mendes, J.2
  • 13
    • 0020547781 scopus 로고
    • A study of short fatigue crack growth Behavior Titanium alloy IMI685
    • BROWN C W, HICKS M A. A study of short fatigue crack growth Behavior Titanium alloy IMI685[J]. Fatigue of Engrg Mater and Struct, 1983, 6(1): 67-76.
    • (1983) Fatigue of Engrg Mater and Struct , vol.6 , Issue.1 , pp. 67-76
    • Brown, C.W.1    Hicks, M.A.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.