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轴流压气机反流状态的实验研究
引用本文:李军,朱俊强,刘红,刘志伟.轴流压气机反流状态的实验研究[J].航空动力学报,1998,13(2):212-214,224.
作者姓名:李军  朱俊强  刘红  刘志伟
作者单位:空军工程学院,西北工业大学
摘    要:依据实验测量结果,本文给出了一单级轴流压气机在反流状态下气动参数沿径向的分布情形,分析了在反流状态下压气机中气流流动的特点。

关 键 词:压气机  气动力试验  流动参数测量
收稿时间:9/1/1997 12:00:00 AM
修稿时间:1997/11/1 0:00:00

EXPERIMENTAL RESEARCH OF REVERSE FLOW IN AXIAL-FLOW COMPRESSOR
Li Jun,Zhu Junqiang,Liu Hong and Liu Zhiwei.EXPERIMENTAL RESEARCH OF REVERSE FLOW IN AXIAL-FLOW COMPRESSOR[J].Journal of Aerospace Power,1998,13(2):212-214,224.
Authors:Li Jun  Zhu Junqiang  Liu Hong and Liu Zhiwei
Institution:1st Dept.Air Force Engineering College,Xi'an 710038;1st Dept.Air Force Engineering College,Xi'an 710038;1st Dept.Air Force Engineering College,Xi'an 710038;7th Dept.Northwestern Polytechnical University,Xi'an 710072
Abstract:The experiments of reverse flow in a single-stage axial-flow compressor were completed.The parameters,such as velocities,static and total pressure,incidence and deviation,were measured at three sections:the inlet section of rotor,the section between rotor and stator,the outlet of stator.The pressures and temperatures of the flow are measured with a steady acquisition system.The experimental results show that,uniform flow parameters are obtained at the outlet section of stator,but the parameters in the inlet section of rotor vary obviously at the radial direction.The incidences of the reverse flow are very large,so there exists a great loss.Therefore,the temeprature rises as the gas flow through the compressor reversely.
Keywords:Compressors  Aerodynamic tests  Flow parameter measurement
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