Analysis of Heat Transfer on the Turbine Blade with Multi-hole Film Cooling
碩士 === 國立交通大學 === 機械工程系所 === 104 === Turbine blades in a gas turbine engine must withstand high temperature and pressure that easily causes the blade broken. In order to protect turbine blades from the situation, a film cooling method has been always employed on the turbine blade. This study simulat...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2016
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| Online Access: | http://ndltd.ncl.edu.tw/handle/15823882413451330888 |