Numerical Thermal Simulation of a Turbine Nozzle with Suction Side Film Cooling
博士 === 國立成功大學 === 航空太空工程學系碩博士班 === 96 === Raising the turbine entry temperature is a common method to increase the performance and power output of a gas turbine engine. However, the level of turbine entry temperature is much higher than the blade material can endure. Thus, it is necessary to guard t...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | en_US |
| Published: |
2008
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| Online Access: | http://ndltd.ncl.edu.tw/handle/10965990495615392002 |