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Analysis of Transonic Flow Fields Inside a High Pressure Ratio Centrifugal Compressor at Design and Off Design Conditions

机译：在设计和关闭设计条件下高压比离心压缩机内延长流场分析

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Chunill Hah; Hartmut Krain;
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年度 1999
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1. Investigation of transient flow characteristics inside a centrifugal compressor for design and off-design conditions [J] . Jiayi Zhao Proceedings of the Institution of Mechanical Engineers . 2018,第4期

机译：在设计和非设计条件下研究离心压缩机内部的瞬态流动特性
2. One-Dimensional and Three- Dimensional Design Strategies for Pressure Slope Optimization of High-Flow Transonic Centrifugal Compressor Impellers [J] . Hildebrandt A., Ceyrowsky T. Journal of turbomachinery . 2019,第5期

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3. EFFECTS OF INLET PRESSURE DISTORTION ON THE PERFORMANCE AND FLOW FIELD OF A CENTRIFUGAL COMPRESSOR AT DESIGN CONDITION [J] . N. Sitaram, M. Govardhan, K.V. Murali Journal of Aerospace Sciences and Technologies . 2012,第4期

机译：设计条件下入口压力畸变对离心压缩机性能和流场的影响
4. DESIGN AND OFF-DESIGN FLOW FIELDS OF A TRANSONIC CENTRIFUGAL COMPRESSOR IMPELLER [C] . Seiichi Ibaraki, Kunio Sumida, Toru Suite ASME turbo expo . 2009

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5. Multi-fidelity Design and Analysis of Single Hub Multirotor High Pressure Centrifugal Compressor [D] . Muppana, Sai. 2018

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6. Stability Improvement of High-Pressure-Ratio Turbocharger Centrifugal Compressor by Asymmetric Flow Control—Part I: Non-Axisymmetrical Flow in Centrifugal Compressor [O] . Mingyang Yang, Xinqian Zheng, Yangjun Zhang, -1

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7. Influences of tip leakage flows on flow field at design condition in transonic centrifugal compressor with splitter blade [O] . Masanao KANEKO, Hoshio TSUJITA 2016

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8. Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.63 and 1.77, respectively, and with design pressure ratio of 2.05 [R] . Moore, R. D., Reid, L. 1982

机译：转子和定子纵横比分别为1.63和1.77，设计压力比为2.05的单级轴流式跨音速压缩机的性能

Analysis of Transonic Flow Fields Inside a High Pressure Ratio Centrifugal Compressor at Design and Off Design Conditions

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