Introduction of residual stresses to enhance fatigue performance in the initial design

Proceedings of the ASME Turbo Expo 2004

Volumn 2, Issue , 2004, Pages 231-239

  Prevéy, Paul ^a   Jayaraman, N ^a   Ravindranath, Ravi ^b  

^a Lambda Technologies   (United States)

^b NAVAL AIR SYSTEMS COMMAND   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPRESSIVE STRESS; COMPRESSORS; EROSION; FRETTING CORROSION; HARDENING; LASERS; MATHEMATICAL MODELS; PITTING; PLASTICITY; RESIDUAL STRESSES; SHOT PEENING; SURFACE TREATMENT; THERMODYNAMIC STABILITY; TURBINES;

HAIGH DIAGRAM; LASER SHOCK PROCESSING (LSP); LOW PLASTICITY BURNISHING (LPB); SURFACE COMPRESSION;

FATIGUE TESTING;

EID: 10244267607     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/gt2004-53971     Document Type: Conference Paper

References (22)

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