Prediction of residual stress distribution after turning in turbine disks

International Journal of Mechanical Sciences

Volumn 48, Issue 9, 2006, Pages 976-984

  Salio, M ^a   Berruti, T ^b   De Poli, G ^c  

^a CENTRO RICERCHE FIAT   (Italy)

^b POLITECNICO DI TORINO   (Italy)

^c AVIO S P A   (Italy)

Author keywords

Finite element; Nickel alloys; Residual stress; Turbine disk; Turning process

Indexed keywords

AIRCRAFT ENGINES; CUTTING; CUTTING FLUIDS; FINITE ELEMENT METHOD; NICKEL ALLOYS; PARAMETER ESTIMATION; RESIDUAL STRESSES; STRESS CONCENTRATION; SURFACE TREATMENT; TURBINES; TURNING;

CUTTING PARAMETERS; FEED RATE; LAGRANGIAN FORMULATION; MSC.SOFTWARE CORPORATION (CO); TURBINE DISK;

DISKS (MACHINE COMPONENTS);

EID: 33744969548     PISSN: 00207403     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ijmecsci.2006.03.009     Document Type: Article

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