Integrated approach for stress based lifing of aero gas turbine blades
In order to analyse the turbine blade life, the damage due to the combined thermal and mechanical loads should be adequately accounted for. This is more challenging when detailed component geometry is limited. Therefore, a compromise between the level of geometric detail and the complexity of the li...
| Main Author: | |
|---|---|
| Other Authors: | |
| Published: |
Cranfield University
2013
|
| Subjects: | |
| Online Access: | http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.600691 |