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Volumn 25, Issue 2, 2002, Pages 99-110

Fatigue life recovery in aluminium alloy aircraft structure

Author keywords

7050 aluminium alloy; Crack growth; Peening; Residual stress

Indexed keywords

AEROSPACE ENGINEERING; AIRCRAFT MATERIALS; AIRFRAMES; CRACK PROPAGATION; FATIGUE OF MATERIALS; RESIDUAL STRESSES; SHOT PEENING; STRESS INTENSITY FACTORS; SURFACE ROUGHNESS; VAPOR DEPOSITION;

EID: 0036466146     PISSN: 8756758X     EISSN: None     Source Type: Journal    
DOI: 10.1046/j.1460-2695.2002.00481.x     Document Type: Article
Times cited : (20)

References (23)
  • 19
    • 0006478778 scopus 로고    scopus 로고
    • F/A-18 FS488 bulk-head fatigue coupon test program
    • DSTO-TR-0941, Department of Defence, Defence Science and Technology Organisation, Aeronautical and Maritime Research Laboratory
    • (2000)
    • Ogden, R.1    Pell, R.2
  • 22
    • 4243604589 scopus 로고    scopus 로고
    • Evaluation of the effect of polished-out surface indentations on the fatigue life of 7050 aluminium alloy
    • Fourth Year Materials Engineering Thesis. Monash University, Melbourne Australia
    • (1997)
    • Turk, S.1
  • 23
    • 77957105960 scopus 로고    scopus 로고
    • Aircraft fatigue life extension; development of a mid-life rework method based on peening
    • ECF13, San Sebastian, Spain, September. (Edited by M. Fuentes, M. Elices, A. Martin Meizoso and J.-M. Martinez-Esnaola, Elsevier Science Ltd., Oxford, UK)
    • (2000) Proceedings of the 13th European Conference on Fracture , pp. 97-114
    • Clark, G.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.