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Volumn 20, Issue 2, 1997, Pages 249-256

Compression fatigue crack growth behaviour of an aluminium alloy: Effect of overloading

Author keywords

Aluminium alloy; Crack tip blunting; Cyclic compression; Fatigue crack growth; Overload; Residual stress

Indexed keywords

ALUMINUM ALLOYS; FATIGUE OF MATERIALS; LOADS (FORCES); RESIDUAL STRESSES;

EID: 0030683169     PISSN: 8756758X     EISSN: None     Source Type: Journal    
DOI: 10.1111/j.1460-2695.1997.tb00282.x     Document Type: Article
Times cited : (5)

References (13)
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  • 3
  • 4
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  • 5
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    • Hermann, R.1
  • 6
    • 0022861997 scopus 로고
    • Fatigue and fracture mechanics analysis of compression loaded aircraft structures
    • ASTM STP 918, Philadelphia
    • D. L. Rich, R. E. Pinckert and T. F. Christian (1986) Fatigue and fracture mechanics analysis of compression loaded aircraft structures: In: Case Histories Involving Fatigue and Fracture Mechanics, ASTM STP 918, pp. 243-258. Philadelphia.
    • (1986) Case Histories Involving Fatigue and Fracture Mechanics , pp. 243-258
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  • 8
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    • Fatigue cracks, fatigue damage and their detection
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    • Christensen, R.H.1
  • 10
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    • Mechanism of overload effect on fatigue crack propagation in aluminium alloys
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    • Bathias, C.1    Vancon, M.2
  • 11
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    • The results of a test programme based on a gust spectrum with variable amplitude loading
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    • (1962) Aircraft Engng , vol.34 , pp. 314-316
    • Schijve, J.1    Broek, D.2
  • 13
    • 0019679139 scopus 로고
    • Crack closure and crack propagation rates in 7050 aluminium
    • D. Gan and J. Weertman (1981) Crack closure and crack propagation rates in 7050 aluminium. Engng Fract. Mech. 15, 87-106.
    • (1981) Engng Fract. Mech. , vol.15 , pp. 87-106
    • Gan, D.1    Weertman, J.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.