Improvement of fatigue property in 7050-T7451 aluminum alloy by laser peening and shot peening

Materials Science and Engineering: A

Volumn 528, Issue 10-11, 2011, Pages 3823-3828

  Gao, Y K ^a  

^a BEIJING INSTITUTE OF AERONAUTICAL MATERIALS   (China)

Author keywords

7050 T7451 aluminum alloy; Fatigue; Laser peening; Residual stresses; Shot peening

Indexed keywords

FATIGUE CRACK PROPAGATION; RESIDUAL STRESSES; SHOT PEENING;

7050-T7451 ALUMINUM ALLOY; COMPRESSIVE RESIDUAL STRESS; FATIGUE CRACKS; FATIGUE PROPERTIES; FATIGUE STRENGTH; LASER PEENING; LASER SHOTS; LOAD CONDITION; RESIDUAL STRESS LAYERS; SHOT-PEENING;

ALUMINUM ALLOYS;

EID: 79952282639     PISSN: 09215093     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.msea.2011.01.077     Document Type: Article

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