Control of Compressor Face Total Pressure Distortion on a High Bypass Turbofan Intake Using Air- Jet Vortex Generators

机译：使用喷气涡流发生器控制高旁路涡轮风扇进气口的压缩机工作面总压变形

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《34th AIAA Fluid Dynamics Conference ; 2nd AIAA Flow Control Conference ; 35th AIAA Plasmadynamics and Lasers Conference ; 37th AIAA Thermophysics Conference》|2004年|P.1-11|共11页
会议地点 Portland OR(US);Portland OR(US);Portland OR(US);Portland OR(US)
作者
S. Erbsloeh; W. Crowther; J. Frutos;
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作者单位

University of Manchester, Manchester, Great Britain;

University of Manchester, Manchester, Great Britain;

Laboratoire de Metrologie des Oscillateurs, Besancon, France;

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原文格式 PDF
正文语种
中图分类流体动力学;
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1. Controlling Separation on a Simulated Compressor Blade Using Vortex-Generator Jets [J] . Simon Evans, Howard Hodson, Tom Hynes, Journal of propulsion and power . 2010,第4期

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2. Controlling Separation on a Simulated Compressor Blade Using Vortex-Generator Jets [J] . Simon Evans Howard Hodson Tom Hynes and Christian Wakelam Journal of Propulsion and Power . 2010,第4期

机译：使用涡发生器喷射器控制模拟压气机叶片的分离
3. Experimental investigation of flow and distortion mitigation by mechanical vortex generators in a coupled serpentine inlet-turbofan engine system [J] . Iman MAGHSOUDI, Mohammad Ali VAZIRY, Mostafa MAHMOODI 中国航空学报（英文版） . 2020,第005期

机译：蛇形进气道-涡轮风扇发动机系统中机械涡流发生器减轻流动和变形的实验研究
4. Control of Compressor Face Total Pressure Distortion on a High Bypass Turbofan Intake Using Air- Jet Vortex Generators [C] . AIAA Fluid Dynamics Conference . 2004

机译：使用空气喷射涡流发电机控制压缩机面部的高旁路涡轮机摄入量的总压力变形
5. Low Pressure Turbine Flow Control with Vortex Generator Jets. [D] . Williams, Charles Phillip Michael. 2016

机译：带有涡流发生器喷嘴的低压涡轮流量控制。
6. Stability Improvement of High-Pressure-Ratio Turbocharger Centrifugal Compressor by Asymmetric Flow Control—Part I: Non-Axisymmetrical Flow in Centrifugal Compressor [O] . Mingyang Yang, Xinqian Zheng, Yangjun Zhang, -1

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7. Separation Control on High Lift Low-Pressure Turbine Airfoils Using Pulsed Vortex Generator Jets [O] . Ralph J. Volino, Mounir B. Ibrahim 2012

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8. Evaluation of an Airjet Distortion Generator Used to Produce Steady-State,Total-Pressure Distortion at the Inlet of a General Electric F101-GE-100Turbofan Engine. [R] . hubble, j. d. smith, r. e. 1979

机译：用于在通用电气F101-GE-100Turbofan发动机进气道产生稳态总压力失真的喷气式失真发生器的评估。

Control of Compressor Face Total Pressure Distortion on a High Bypass Turbofan Intake Using Air- Jet Vortex Generators

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