Surface layer properties and fatigue behavior in Al 7075-T73 and Ti-6Al-4V Comparing results after laser peening; Shot peening and ball-burnishing

International Journal of Structural Integrity

Volumn 2, Issue 2, 2011, Pages 185-199

  Wagner, Lothar ^a   Mhaede, Mansour ^a,b   Wollmann, Manfred ^a   Altenberger, Igor ^c   Sano, Yuji ^d  

^a CLAUSTHAL UNIVERSITY OF TECHNOLOGY   (Germany)

^b Zagazig University   (Egypt)

^c Hochschule Berlin   (Germany)

^d TOSHIBA CORPORATION   (Japan)

Author keywords

Aircraft; Alloys; Fatigue; Stress (materials); Surface treatment

Indexed keywords

AIRCRAFT ALLOYS; BALL-BURNISHING; DESIGN/METHODOLOGY/APPROACH; FATIGUE; FATIGUE BEHAVIOR; FATIGUE LIFE; FATIGUE PERFORMANCE; FATIGUE STRENGTH; FULLY REVERSED; LASER PEENING; MECHANICAL SURFACE TREATMENT; REFERENCE CONDITION; ROTATING BEAM; STRESS (MATERIALS); SURFACE LAYERS; TI-6AL-4V; ULTRASONIC SHOT PEENING;

AIRCRAFT; AIRCRAFT MATERIALS; ALLOYS; ALUMINUM; BURNISHING; CERIUM ALLOYS; FATIGUE OF MATERIALS; MECHANICAL PROPERTIES; SHOT PEENING; STRESSES; SURFACE PROPERTIES; SURFACE ROUGHNESS; TITANIUM ALLOYS;

SURFACE TREATMENT;

EID: 79957813525     PISSN: 17579864     EISSN: 17579872     Source Type: Journal    
DOI: 10.1108/17579861111135923     Document Type: Article

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