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47篇 您的检索式：作者名="FOTTNER L"

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	题名	作者	年代	出处	被引量
1	Improved blade profile loss and deviation angle models for advanced transonic compressor bladeings Part Ⅱ-A model for supersonic flow显示文摘	Konig W M Hennecke D K Fottner L	1996	Journal of Turbomachinery1996，11，：	1
2	A numerical study of the influ- ence of grid refinement and turbulence modeling on the flow inside a highly loaded turbine cascade显示文摘	Hilderbrandt T Fottner L	1999	Journal of Turbomachinery1999，121，4：	1
3	Influence of taper, Reynolds number and Mach number on the secondary flow field of a highly loaded turbine cascade显示文摘	Duden A Fottner L	1997	Journal of Power and Energy1997，211，4：	1
4	The Influence of Transients Inlet Distortions on the Instability Uneeption of a Low - pressure Compressor in a Turbofan Engine显示文摘	Leinhos D Sehmid N R Fottner L	2001	ASME J of Turbomachinery2001，123，1：	1
5	The influence of load distribution on secondary flow in straight turbine cascades显示文摘	Weiss P Fottner L	1995	J Turbomachinery1995，117，1：	1
6	The influence of load distribution on secondary flow in straight turbine cascades显示文摘	WEISS P FOTTNER L	1995	ASME Journal of Turbomachinery1995，117，：	1
7	Bone metastases from renal cell carcinoma:patient survival after surgical treatment显示文摘	Fottner A Szalantzy M Wirthmann L	2010	BMC Musculoskelet Disord2010，11，：	1
8	Improved blade profile loss and deviation angel models for advanced transonic compressor bladeings: Part 2-a model for supersonic flow显示文摘	Konig W M Hennecke D K Fottner L	1996	ASME Journal of Turbomanchinery1996，117，1：	1
9	Stall Inception in the Compressor System of a Turbofan Engine显示文摘	Hoss B Leinhos D Fottner L	2000	ASME J Turbomachinery2000，122，1：	1
10	The influence of transient inlet distortions on the instability inception of a low-pressure compressor in a turbofan engine显示文摘	Leinhos D C Schmid N R Fottner L	2001	Journal of Turbomachinery2001，123，1：	1
11	Boundary Layer Investigations on a Highly Loaded Transonic Compressor Cascade with Shock/Laminar Boundary l,ayer Interac- tions 显示文摘	Hilgenfeld 1~ Cardamone P Fottner L	2003	Proceedings of' the Institution o[' Mechanical Engineers Part A: Journal of Power and Energy2003，217，4：	1
12	Improved blade profile loss and deviation angle models for advanced transonic compressor bladings: Part Ⅰ: A model for subsonic flow显示文摘	Konig W M Henneck D K Fottner L	1996	Journal of Turbomachinery1996，117，：	1
13	Stall inception in the compressor system of a turbo fan engine 显示文摘	Hoss B Leinhos D Fottner L	1998	Journal of Turbomachinery1998，120，1：	1
14	Improved blade profile loss and deviation angle models for advanced transonic compressor bladings: Part Ⅱ:A model for supersonic flow显示文摘	Konig W M Henneek D K Fottner L	1996	Journal of Turbomachinery1996，118，：	1
15	The influence of load distribution on secondary flow in straight turbine cascades 显示文摘	WEISS P FOTTNER L	1995	ASME Jourrnal of Turbomachinery1995，117，：	1
16	Improved blade profile loss and deviation angel models for advanced transonic compressor bladings:Part Ⅰ-a model for subsonic flow显示文摘	Konig W M Hennecke D K Fottner L	1996	Transactions of the ASME Journal of Turbomachinery1996，117，1：	1
17	Improved blade profile loss and deviation angel models for advanced transonic compressor bladings:Part Ⅱ-a model for supersonic flow显示文摘	Konig W M Hennecke D K Fottner L	1996	Transactions of the ASME Journal of Turbomachinery1996，117，1：	1
18	Bone metastases from renal cell carcinoma:patient survival after surgical treatment显示文摘	Fottner A Szalantzy M Wirthmann L	2010	BMC Musculoskelet Disord2010，11，：	1
19	Stall Inception in the Com- pressor System of a Turbofan Engine显示文摘	Hoss B Leinhos D Fottner L		0，，01：	1
20	The Influence of Transient Inlet Distortions on the Instability Inception of A Low - Pressure Compressor in A Turbofan Engine显示文摘	Leinhos D Schmid N R Fottner L	2001	ASME J Turbomachinery2001，123，1：	1

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