中国科学院机构知识库网格系统: 检索

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	Active Stabilization of the Compression System in a Twin-spool Turbofan Engine at Inlet Distortions 会议论文 OAI收割 ISABE, 2003 S.G.Scheidler; L.Fottner 收藏 \| 浏览/下载：7/0 \| 提交时间：2013/09/04
	Optimization of Three Dimensional Designed Turbine Blades and Side Walls 会议论文 OAI收割 ISABE, 2001 M.G.Nagel; L.Fottner; R-D.Baier 收藏 \| 浏览/下载：39/0 \| 提交时间：2013/09/04
	STALL INCEPTION IN THE COMPRESSOR SYSTEM OF A TURBOFAN ENGINE 会议论文 OAI收割 ASME, Stockholm,Sweden B.Höss; D.Leinhos; L.Fottner 收藏 \| 浏览/下载：11/0 \| 提交时间：2012/07/12
	IMPROVED BLADE PROFILE LOSS AND DEVIATION ANGLE MODELS FOR ADVANCED TRANSONIC COMPRESSOR BLADINGS: PART II -A MODEL FOR SUPERSONIC FLOW 会议论文 OAI收割 ASME, The Hague, Netherlands, 1994-06-13 W.M. König; D.K. Hennecke; L.Fottner 收藏 \| 浏览/下载：16/0 \| 提交时间：2012/08/06
	IMPROVED BLADE PROFILE LOSS AND DEVIATION ANGLE MODELS FOR ADVANCED TRANSONIC COMPRESSOR BLADINGS:PART I - A MODEL FOR SUBSONIC FLOW 会议论文 OAI收割 ASME, The Hague, Netherlands, 1994-06-13 W.M.Konig and D.K.Hennecke; L.Fottner 收藏 \| 浏览/下载：12/0 \| 提交时间：2012/08/06
	IMPROVED BLADE PROFILE LOSS AND DEVIATION ANGLE MODELS FOR ADVANCED TRANSONIC COMPRESSOR BLADINGS:PART I - A MODEL FOR SUBSONIC FLOW 会议论文 OAI收割 The Hague, Netherlands, 1994-06-13 作者: W.M.Konig and D.K.Hennecke; L.Fottner \| 收藏 \| 浏览/下载：11/0 \| 提交时间：2012/08/06
	IMPROVED BLADE PROFILE LOSS AND DEVIATION ANGLE MODELS FOR ADVANCED TRANSONIC COMPRESSOR BLADINGS: PART II -A MODEL FOR SUPERSONIC FLOW 会议论文 OAI收割 The Hague, Netherlands, 1994-06-13 作者: W.M. König; D.K. Hennecke; L.Fottner \| 收藏 \| 浏览/下载：11/0 \| 提交时间：2012/08/06
	EXPERIMENTAL INVESTIGATIONS OF THE INFLUENCE OF INCOMING WAKES ON THE LOSSES OF A LINEAR TURBINE CASCADE 会议论文 OAI收割 ASME, Cincinnati,Ohio M.Ladwing; L.Fottner 收藏 \| 浏览/下载：3/0 \| 提交时间：2012/08/06