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Unsteady Flow Field under Surge and Rotating Stall in a Three-stage Axial Flow Compressor

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摘要在在一台三阶段的轴的流动压缩机的转子blade-to-blade段落之间的不稳定的流动结构被不稳定的表演特征，casing墙压力变化和他们的小浪分析的详细大小试验性地调查。测试压缩机的主要特征是在系列连接到压缩机插头以便供应压缩或扩大波浪从的一台能力坦克设备压缩机下游。研究注意集中于同时发生的巨浪和旋转货摊的货摊以后的特征。在不稳定的表演曲线上操作点的压缩机的影响证明巨浪周期不规则地变化取决于不变的抵抗特征，并且墙压力变化的小浪分析的结果建议巨浪周期可以被旋转货摊房间结构有选择地在转子串联以内决定。

DOI 5jook8ykjv/944612

作者 Takayuki HARA;Daisuke MORITA;Yutaka OHTA;Eisuke OUTA

机构地区不详

出处《热科学学报：英文版》 2011年1期

关键词轴流压缩机非定常流场旋转失速三阶喘振转子叶片

分类 [理学][物理]

出版日期 2011年01月11日（中国期刊网平台首次上网日期，不代表论文的发表时间）

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来源期刊

热科学学报：英文版

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轴流压缩机非定常流场旋转失速三阶喘振转子叶片

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