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Volumn 27, Issue 3, 2005, Pages 245-253

Innovative laser heating methodology study for crack growth retardation in aircraft structures

Author keywords

Crack growth retardation; Fatigue; Laser heating; Microstructure; Residual stress

Indexed keywords

AGING OF MATERIALS; CARBON DIOXIDE LASERS; CRACK PROPAGATION; FATIGUE OF MATERIALS; HEATING; MICROSTRUCTURE; PARAMETER ESTIMATION; RESIDUAL STRESSES; SAMPLING; TENSILE STRESS;

EID: 10444282136     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ijfatigue.2004.07.003     Document Type: Article
Times cited : (9)

References (19)
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  • 11
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    • Laser shock processing and its effects on microstructure and properties of metal alloys: A review
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    • Montross, C.S.1    Wei, T.2    Ye, L.3    Clark, G.4    Mai, Y.W.5
  • 12
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    • Laser shock processing increases the fatigue life of metal parts
    • Clauer AH, Koucky JR. Laser shock processing increases the fatigue life of metal parts. Mater Process 1991;6:3-5.
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    • Effect of simultaneous overload and spot heating on crack growth retardation in fatigue
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    • Method for reducing the fatigue crack growth rate of cracks in the aluminum alloy fuselage skin of an aircraft structure. United States Patent, Patent No. 5071492; Dec 10
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.