Finite Volume Based Numerical Investigation On The Effects Of Internal Cooling And Film Cooling On The Thermal Performance Of Gas Turbine Blades
The inlet temperature of modern gas turbine engines has been increased to achieve higher thermal efficiency and increased output. The blade surfaces including the leading edge, suction side and pressure side are exposed to the most extreme heat loads, and therefore, must be adequately cooled to main...
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| 格式: | Thesis |
| 语言: | English |
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2010
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| 在线阅读: | http://eprints.usm.my/42736/1/SUFIAN_FARID_SHAKER.pdf |
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