Numerical modelling of creep deformation in a CMSX-4 single crystal superalloy turbine blade
The creep deformation behaviour of a high pressure (cooled) turbine blade section is modelled using the finite element method. Realistic estimates of the thermal and mechanical loading expected during service are employed; properties for the single crystal superalloy CMSX-4 are assumed. The constitu...
Main Authors: | Dye, D, Ma, A, Reed, R |
---|---|
Format: | Journal article |
Language: | English |
Published: |
2008
|
Similar Items
-
A model for the creep deformation behaviour of single-crystal superalloy CMSX-4
by: Ma, A, et al.
Published: (2008) -
Recrystallization of single crystal superalloy CMSX-4 casting
by: XU Fuze, et al.
Published: (2023-10-01) -
Numerical and experimental study of post-heat treatment gas quenching and its impact on microstructure and creep in CMSX-10 superalloy
by: Cosentino, F, et al.
Published: (2013) -
The Influence of the Cooling Bores on the Dendritic Structure and Crystal Orientation in Single-Crystalline Cored CMSX-4 Turbine Blades
by: Jacek Krawczyk, et al.
Published: (2021-07-01) -
The Low-Angle Boundaries Misorientation and Lattice Parameter Changes in the Root of Single-Crystalline CMSX-4 Superalloy Blades
by: Robert Paszkowski, et al.
Published: (2021-09-01)