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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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書目詳細資料
主要作者:	Tan, Kien Weng
格式:	Final Year Project
出版:	Universiti Teknologi Petronas 2009
主題:	TJ Mechanical engineering and machinery
在線閱讀:	http://utpedia.utp.edu.my/662/
標簽:	添加標簽沒有標簽, 成為第一個標記此記錄!

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