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Volumn 12, Issue 4, 2005, Pages 586-603

The comparison of complex load sequences tested at several stress levels by fractographic examination

Author keywords

Crack growth; Fatigue crack growth; Fatigue life; Load history; Surface finish

Indexed keywords

AIRCRAFT; ALUMINUM ALLOYS; FATIGUE OF MATERIALS; FRACTOGRAPHY; STRESSES;

EID: 17644378007     PISSN: 13506307     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.engfailanal.2004.09.007     Document Type: Article
Times cited : (27)

References (14)
  • 1
    • 0006478778 scopus 로고    scopus 로고
    • F/A-18 FS488 bulkhead fatigue coupon test program
    • Defence Science and Technology Organisation, DSTO-TR-0941, Australia
    • Molent L, Ogden R, Pell R. F/A-18 FS488 bulkhead fatigue coupon test program. Defence Science and Technology Organisation, DSTO-TR-0941, Australia; 2000
    • (2000)
    • Molent, L.1    Ogden, R.2    Pell, R.3
  • 2
    • 0006478778 scopus 로고    scopus 로고
    • F/A-18 FS488 bulkhead fatigue coupon test program
    • Defence Science and Technology Organisation, DSTO-TR-1464, July
    • Molent L, Mills T, Pell R. F/A-18 FS488 bulkhead fatigue coupon test program - part 2. Defence Science and Technology Organisation, DSTO-TR-1464, July; 2003
    • (2003) , Issue.PART 2
    • Molent, L.1    Mills, T.2    Pell, R.3
  • 3
    • 7444247091 scopus 로고    scopus 로고
    • The fractographical comparison of F/A-18 aluminium alloy 7050-T7451 bulkhead representative coupons tested under two fatigue load spectra at several stress levels
    • DSTO-TR-1547, February
    • Pell RA, Molent L, Green AJ. The fractographical comparison of F/A-18 aluminium alloy 7050-T7451 bulkhead representative coupons tested under two fatigue load spectra at several stress levels. DSTO-TR-1547, February; 2004
    • (2004)
    • Pell, R.A.1    Molent, L.2    Green, A.J.3
  • 4
    • 17644379969 scopus 로고    scopus 로고
    • Validation of fatigue damage models used for F/A-18 life assessment using fatigue coupon test results
    • Defence Science and Technology Organisation, DSTO-TR-0940, Australia
    • Dickinson T, Molent L. Validation of fatigue damage models used for F/ A-18 life assessment using fatigue coupon test results. Defence Science and Technology Organisation, DSTO-TR-0940, Australia; 2000
    • (2000)
    • Dickinson, T.1    Molent, L.2
  • 6
    • 17644389222 scopus 로고    scopus 로고
    • Validation against coupon test results of the fatigue damage model CI89 for F/A-18 aft fuselage and empennage spectra
    • Defence Science and Technology Organisation, DSTO-TR-1292, Australia
    • Molent L, Mau VT. Validation against coupon test results of the fatigue damage model CI89 for F/A-18 aft fuselage and empennage spectra. Defence Science and Technology Organisation, DSTO-TR-1292, Australia; 2002
    • (2002)
    • Molent, L.1    Mau, V.T.2
  • 7
    • 17644375519 scopus 로고    scopus 로고
    • Coupon tests to determine the influence of buffet detected at the F/A-18 wing root
    • Defence Science and Technology Organisation, DSTO-TR-0924, Australia
    • Aktepe B, Dickinson T. Coupon tests to determine the influence of buffet detected at the F/A-18 wing root. Defence Science and Technology Organisation, DSTO-TR-0924, Australia; 2000
    • (2000)
    • Aktepe, B.1    Dickinson, T.2
  • 11
    • 17644411705 scopus 로고    scopus 로고
    • A comprehensive guide to the fatigue damage assessment computer program CI89
    • DSTO-TR-1506, October
    • Ghidella JR, Molent L, Madley WB. A comprehensive guide to the fatigue damage assessment computer program CI89, DSTO-TR-1506, October; 2003
    • (2003)
    • Ghidella, J.R.1    Molent, L.2    Madley, W.B.3
  • 12
    • 17644371697 scopus 로고
    • Coupon fatigue test comparisons of US and Australian F/A-18 bulkhead sequences
    • Defence Science and Technology Organisation, DSTO-TM- 546, Australia
    • Finney JM. Coupon fatigue test comparisons of US and Australian F/A-18 bulkhead sequences. Defence Science and Technology Organisation, DSTO-TM- 546, Australia; 1991
    • (1991)
    • Finney, J.M.1
  • 13
    • 0006468243 scopus 로고
    • Defect assessment on F/A-18 488 bulkhead tested at ARL
    • Defence Science and Technology Organisation, Aircraft Material Report 125, Australia
    • Barter SA, Bishop B, Clark G. Defect assessment on F/A-18 488 bulkhead tested at ARL. Defence Science and Technology Organisation, Aircraft Material Report 125, Australia; 1991
    • (1991)
    • Barter, S.A.1    Bishop, B.2    Clark, G.3
  • 14
    • 0006397475 scopus 로고    scopus 로고
    • Fractographic inspection of the cracking FT488/2 removed at program 79
    • Defence Science and Technology Organisation, DSTO-TN-0170, Australia
    • Barter SA. Fractographic inspection of the cracking FT488/2 removed at program 79. Defence Science and Technology Organisation, DSTO-TN-0170, Australia; 1998
    • (1998)
    • Barter, S.A.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.