维普期刊资源整合服务平台（V6.5）

53篇 您的检索式：作者名="Mailach"

选中清除导出查看参考文献查看引证文献引用追踪共3页首页上一页第1页下一页末页 /3 跳转

	题名	作者	年代	出处	被引量
1	Aerodynamic blade row interactionin an axial compressor: Part U unsteady profile pressuredistribution and blade forces显示文摘	Mailach R Vogeler K	2004	Journal of Turbomachin-ery2004，126，1：	1
2	Rotor-stator interactionsin a four-stage low-speed axial compressor: Part H un-steady aerodynamic forces of rotor and stator blades显示文摘	Mailach R Muller L Vogeler K	2004	Journal of Turbomachinery2004，126，4：	1
3	Periodical Un- steady Flow within a Rotor Blade Row of an Axial Cons- pressor-Part Ⅱ : Wake-Tip Clearance Vortex Interaction 显示文摘	Mailach R Lehmann I Vogeler K	2008	Journal of Turbomachinery2008，130，4：	1
4	Rotating instabilities in an axial compressor originating from the fluctuating blade tip vortex显示文摘	Mailach R Lehmann I Vogeler K	2001	Journal of Turbomachinery2001，123，3：	1
5	Rotating Instabilities in an Axial Compressor Originating from the Fluctuating Blade Tip Vortes 显示文摘	Mailach R Lehmann I Vogeler K	2001	ASME Journal of Turbomachinery2001，123，3：	1
6	Aerodynamic blade row interactions in an axial compressor, part I : unsteady boundary layer develop- ment显示文摘	Mailach R Vogeler K	2004	ASME Jourmal of Turbomachinery2004，126，1：	1
7	Aerodynamic blade row interactions in an axial compressor, part II :unsteady profile pressure distrub- tion and blade forces显示文摘	Mailach R Vogeler K	2004	ASME Jourmal of Turbomachinery2004，126，1：	1
8	Rotor-stator interactions in a four-stagelow-speed axial compressor----part I : unsteady profile pressuresand the effect of clocking 显示文摘	Mailach R Vogeler K	2004	ASME Journal of Turboraachinery2004，126，10：	1
9	Aerodynamic blade row interactions in an axial compressor:Part I- Unsteady boundary layer development显示文摘	Mailach R Vogeler K	2004	ASME Journal of Turbomachinery2004，126，1：	1
10	Unsteady Blade Loading with Clocking in Multistage Axial Compressors, Part 2显示文摘	Lutz Muller Ronald Mailach Konrad Vogeler Huixia Jia	2010	Journal of Propulsion and Power2010，26，1：	1
11	Aerodynamic blade row interactions in an axial compressor:Part II -Unsteady profile pressure distribution and blade forces显示文摘	Mailach R Vogeler K	2004	ASME Journal of Turbomachinery2004，126，1：	1
12	Rotating instabilities in an axial compressor originating from the fluctuating blade tip vortex 显示文摘	MAILACH R LEHMANN I VOGELER K	2000	Journal of turbomachi- nery2000，123，3：	1
13	Rotating instabilities in an axial compressor originating from the fluctuating blade tip vortex显示文摘	MAILACH R LEHMANN I VOGELER K	2001	Journal of Turbomachinery2001，123，3：	1
14	Periodical unsteady flow within a rotor blade row of an axial compressor:Part Ⅰ flow field at midspan显示文摘	Mailach R Lehmann I Vogeler K	2008	Journal of Turbomachinery2008，130，4：	1
15	Periodical unsteady flow within a rotor blade row of an axial compressor:Part Ⅱ wake-tip clearance vortex interaction显示文摘	Mailach R Lehmann I Vogeler K	2008	Journal of Turbomachinery2008，130，4：	1
16	Rotating instabilities in an axial compressor originating from the fluctuating blade tip vortex 显示文摘	Mailach R Lehmann 1 Vogeler K	2001	ASME Journal of Turbomaehinery2001，123，3：	1
17	Periodical unsteady flow within a rotor blade row of an axial compressor Part II: wake tip clearance vortex interaction显示文摘	Mailach R Lehmann I Vogeler K	2008	Journal of Turbomachinery2008，130，4：	1
18	Aerodynamic blade row interactions in an axial compressor: Part I unsteady boundary layer development 显示文摘	Mailach R Vogeler K	2004	Jourmal of Turbomachinery2004，126，1：	1
19	Aerodynamic blade row interactions in an axial compressor: Part II unsteady profile pressure distrubtion and blade forces 显示文摘	Mailach R Vogeler K	2004	Jourmal of Turbomaehinery2004，126，1：	1
20	Rotating Instabilities in an Axial Compressor Originating from the Fluctuating Blade Tip Vortex显示文摘	Mailach R Lehmann I Vogeler K		0，，：	1

返回顶部每页显示：

共3页首页上一页第1页下一页末页 /3 跳转

互联网出版许可证新出网证(渝)字10号全国400电话 - 免长途话费

用户提示