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二维轴流压气机转—静非定常Euler方程数值计算
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作者 葛宁 《航空动力学报》 EI CAS CSCD 北大核心 2000年第1期35-38,共4页
将Euler方程写在包括转子和静子的绝对坐标系下,通过在转—静之间设计一个可以随时间扭动的平行四边形网格计算了二维轴流压气机转—静非定常流场。由于整个方程统一写在动网格下,转—静之间没有使用插值。
关键词 非定常流场轴流 压气机 数值计算 EULER方程
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Unsteady Flow Field under Surge and Rotating Stall in a Three-stage Axial Flow Compressor 被引量:5
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作者 Takayuki HARA Daisuke MORITA +1 位作者 Yutaka OHTA Eisuke OUTA 《Journal of Thermal Science》 SCIE EI CAS CSCD 2011年第1期6-12,共7页
The unsteady flow structure between rotor blade-to-blade passages in a three-stage axial flow compressor is experimentally investigated by detailed measurements of unsteady performance characteristics,casing wall pres... The unsteady flow structure between rotor blade-to-blade passages in a three-stage axial flow compressor is experimentally investigated by detailed measurements of unsteady performance characteristics,casing wall pressure fluctuations and their wavelet analyses.The main feature of the test compressor is a capacity tank facility connected in series to the compressor outlet in order to supply compression and/or expansion waves from downstream of the compressor.Research attention is focused on the post-stall characteristics of the surge and rotating stall which occur simultaneously.The influence of the compressor operating point on the unsteady performance curve shows that the surge cycle changes irregularly depending on the steady-state resistance characteristics,and the results of the wavelet analyses of the wall pressure fluctuations suggest that the surge cycle may selectively be determined by the rotating stall cell structure within the rotor cascade. 展开更多
关键词 Axial flow compressor SURGE Rotating stall Stall cell Wavelet analysis.
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