Simulation And Flow Characterization Of Spiked Supersonic Gas Turbine Intake At Non-Zero Angle Of Attack
Intake of a supersonic gas turbine requires the highest possible total pressure recovery and minimal total pressure lost in order to obtain an efficient operation. The supersonic intake is mainly affected by two substantial factors which are the angle of attack and the geometry of the spike (wedge a...
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| フォーマット: | Final Year Project |
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Universiti Teknologi Petronas
2009
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| オンライン･アクセス: | http://utpedia.utp.edu.my/662/ |
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