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Experimental investigation of the effect of circumferential inlet flow distortion on the performance of a five-stage axial-flow research compressor with transonic rotors in all stages

机译：周向入口流动变形对跨级转子五级轴流研究压缩机性能影响的实验研究

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Robbins, William H; Glaser, Frederick;
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年度 1958
页码 1-105
总页数 105
原文格式 PDF
正文语种 eng
中图分类工业技术;
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入库时间 2022-08-29 11:19:14

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2. Numerical Investigation of Inlet Distortion on an Axial Flow Compressor Rotor with Circumferential Groove Casing Treatment [J] . Huang Jian, Wu Hu 中国航空学报（英文版） . 2008,第006期

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3. Non-uniform stator loss reduction design strategy in a transonic axial-flow compressor stage under inflow distortion [J] . Lu Hanan, Yang Zhe, Pan Tianyu, Aerospace science and technology . 2019,第SEPa期

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4. AN EXPERIMENTAL INVESTIGATION ABOUT THE EFFECT OF THE PARTIAL CASING TREATMENT ON A TRANSONIC AXIAL-FLOW COMPRESSOR PERFORMANCE UNDER INLET DISTORTION [C] . Maoyi Li, Wei Yuan, Xizhen Song, ASME turbo expo . 2012

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5. Numerical Investigation on the Effects of Self-Excited Tip Flow Unsteadiness and Blade Row Interactions on the Performance Predictions of Low Speed and Transonic Compressor Rotors. [D] . Lee, Daniel H. 2013

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6. Effect of Inlet Air Volumetric Flow Rate on the Performanceof a Two-Stage Cyclone Separator [O] . Jihe Chen, Zhong-an Jiang, *, 2018

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7. Discussion: “Aerodynamic Design and Performance of Five-Stage Transonic Axial-Flow Compressor” (Kovach, Karl, and Sandercock, D. M., 1961, ASME J. Eng. Power, 83, pp. 303–320) [O] . P. Schwaar 1961

机译：讨论：“五阶段跨音轴流式压缩机的空气动力学设计和性能”（Kovach，Karl和Sandercock，D. M.，1961，Asme J. Eng。Power，83，PP。303-320）

Experimental investigation of the effect of circumferential inlet flow distortion on the performance of a five-stage axial-flow research compressor with transonic rotors in all stages

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