Blade Design and Thrust Performance for a Miniature Turbojet Engine

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题名:	Blade Design and Thrust Performance for a Miniature Turbojet Engine
作者:	蔡博章 Tsai, Bor-Jang
贡献者:	機械工程學系 Mechanical Engineering
关键词:	Compressor;Turbine;Combustor;Blade Design;Trust;Small Turbojet Engine Compressor;Turbine;Combustor;Blade Design;Trust;Small Turbojet Engine
日期:	2006
上传时间:	2014-06-27 03:10:07 (UTC+8)
摘要:	The development of an axial-flow turbine and centrifugal compressor for P60 engine which is a small, low cost, 50-lbf-thrust turbojet engine, with a single-shaft turbojet with a bell-mouth inlet, a single-stage mixed-flow compressor, a through-flow annula The development of an axial-flow turbine and centrifugal compressor for P60 engine which is a small, low cost, 50-lbf-thrust turbojet engine, with a single-shaft turbojet with a bell-mouth inlet, a single-stage mixed-flow compressor, a through-flow annula
显示于类别:	[機械工程學系] 期刊論文

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