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Journal of Materials Engineering and Performance

Volumn 10, Issue 6, 2001, Pages 670-678

Introduction of compressive residual stresses in Ti-6Al-4V simulated airfoils via laser shock processing

(4) Ahrens, B a,b Linden, M a,b Zaske H a,b Berzewski, H a,b

a FREIE UNIVERSITÄT BERLIN (Germany)

b UNIVERSITY OF LÜBECK (Germany)

Author keywords

Component surface treatment; Laser shock processing; LSP; Residual stress; Ti 6Al 4V

Indexed keywords

COMPRESSIVE STRESS; CRACK PROPAGATION; FATIGUE OF MATERIALS; LASER APPLICATIONS; METALLOGRAPHY; MICROSTRUCTURE; NONDESTRUCTIVE EXAMINATION; RESIDUAL STRESSES; SCANNING ELECTRON MICROSCOPY; ULTRASONIC APPLICATIONS; X RAY DIFFRACTION ANALYSIS;

LASER POWER DENSITY; LASER SHOCK PROCESSING (LSP);

AIRFOILS;

EID: 0035576993 PISSN: 10599495 EISSN: None Source Type: Journal
DOI: 10.1361/105994901770344539 Document Type: Article

Times cited : (34)

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