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: | , , |
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| Format: | Journal article |
| Language: | English |
| Published: |
2008
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