Simplification of 3d cooled turbine blade models for efficient dynamic analyses
In gas turbines, the temperature behind the combustors is the highest, meaning that the blades in the first stage of the turbine require cooling air. This makes the structural blade model very detailed due to the presence of the cooling pattern. For aeromechanical design, one of the first steps is t...
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| Format: | Others |
| Language: | English |
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KTH, Kraft- och värmeteknologi
2013
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-140603 |