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Laser Two-Focus Anemometry Investigation of the Flow Field Within a Supersonic Axial Compressor Rotor

机译：超音速轴向压缩机转子内的流场的激光两对焦风光测定

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Isabelle Trebinjac; André Vouillarmet;
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1. Periodical Unsteady Flow Within A Rotor Blade Row Of An Axial Compressor-part Ⅰ: Flow Field At Midspan [J] . Ronald Mailach, Ingolf Lehmann, Konrad Vogeler Journal of turbomachinery . 2008,第4期

机译：轴流压气机转子叶片行内的非定常周期性流动（Ⅰ）：中跨流场
2. IMPACTS OF TIP CLEARANCE SIZE VARIATION IN DIFFERENT ROTORS ON THE OVERALL PERFORMANCE AND UNSTEADY FLOW FIELDS IN A COUNTER-ROTATING AXIAL FLOW COMPRESSOR [J] . Hang Zhao, Bo Liu, Xiaochen Mao Journal of Aeronautics Astronautics and Aviation . 2017,第4期

机译：反向旋转轴流压缩机中不同转子的尖端间隙尺寸变化对整体性能和非定常流场的影响
3. IMPACTS OF TIP CLEARANCE SIZE VARIATION IN DIFFERENT ROTORS ON THE OVERALL PERFORMANCE AND UNSTEADY FLOW FIELDS IN A COUNTER-ROTATING AXIAL FLOW COMPRESSOR [J] . Hang Zhao, Bo Liu, Xiaochen Mao Journal of Aeronautics, Astronautics and Aviation, A . 2017,第4期

机译：尖端间隙尺寸变化在逆旋转轴流压缩机中的整体性能和非定常流场上的影响
4. PERIODICAL UNSTEADY FLOW WITHIN A ROTOR BLADE ROW OF AN AXIAL COMPRESSOR - PART Ⅰ: FLOW FIELD AT MIDSPAN [C] . Ronald Mailach, Ingolf Lehmann, Konrad Vogeler ASME(American Society of Mechanical Engineers) Turbo Expo vol.6 pt.B; 20070514-17; Montreal(CA) . 2007

机译：轴流压气机转子叶片行内的周期性非定常流动-第一部分：中跨流场
5. Experimental investigation of the flow field in a transonic, axial flow compressor with respect to the development of blockage and loss [D] . Suder, Kenneth Lee 1996

机译：跨音速轴流式压缩机流场关于阻塞和损失发展的实验研究
6. Development of a PVDF Sensor Array for Measurement of the Dynamic Pressure Field of the Blade Tip in an Axial Flow Compressor [O] . Jiqing Cong, Jianping Jing, Changmin Chen, 2019

机译：PVDF传感器阵列的开发用于测量轴流压缩机中叶尖的动态压力场
7. Studies on the flow in supersonic axial-flow compressor rotor. (Part 6) A possibility of two-dimensional supersonic portion having quasi-axisymmetric flows which satisfy simplified radial equilibrium. [O] . Takaaki HASHIMOTO, Shintaro OTSUKA 1984

机译：超音速轴流压缩机转子流动研究。（第6部分）具有具有拟轴对称流的二维超声波部分，其满足简化的径向平衡。
8. Investigation of a One Stage Axial Flow Supersonic Compressor, Part 1. Global Performance of the Blunt Trailing Edge Blade Rotor R 32 [R] . Breugelmans, F. 1965

机译：单级轴流超音速压缩机的研究，第1部分。钝后缘叶片转子R 32的全局性能

Laser Two-Focus Anemometry Investigation of the Flow Field Within a Supersonic Axial Compressor Rotor

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