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Undistorted inlet flow testing. Evaluation of range and distortion tolerance for high Mach number transonic fan stages, volume 2 Task 2 stage data and performance report

机译：无扭曲的入口流量测试。评估高马赫数跨音速风扇级的范围和失真容差，第2卷任务2阶段数据和性能报告

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Evaluation of range and distortion tolerance for high Mach number transonic fan stages - Vol. 2

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Bilwakesh, K. R.;
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年度 1971
页码 1-290
总页数 290
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
COMPRESSOR BLADES; ENGINE DESIGN; TURBOCOMPRESSORS; FLOW DISTRIBUTION; GAS FLOW; PERFORMANCE TESTS;

机译：压缩机叶片;发动机设计;涡轮压缩机;流量分配;气流;性能测试;

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1. Design and performance analysis of a two-stage transonic low-reaction counter-rotating aspirated fan/compressor with inlet counter-swirl [J] . Sun Shijun, Wang Songtao, Zhang Longxin, Aerospace science and technology . 2021,第Apra期

机译：两级跨音速低反应反旋转吸气式风扇/压缩机的设计与性能分析
2. The Effect of Inlet Guide Vanes on Inlet Flow Distortion Transfer and Transonic Fan Stability [J] . M. J. Shaw, P. Hield, P. G. Tucker Journal of turbomachinery . 2014,第2期

机译：进口导流叶片对进口流量畸变传递和跨音速风扇稳定性的影响
3. Influences of flow loss and inlet distortions from radial inlets on the performances of centrifugal compressor stages [J] . Han Fenghui, Mao Yijun, Tan Jiajian Journal of Mechanical Science and Technology . 2016,第10期

机译：径向入口的流量损失和入口变形对离心压缩机级性能的影响
4. UNSTEADY METHODS TO INVESTIGATE INLET DISTORTION IN A TRANSONIC TAIL CONE THRUSTER FAN STAGE WITH BOUNDARY LAYER INGESTION [C] . Ritangshu Giri, Mark G. Turner, Mark L. Celestina ASME Turbo Expo: Turbomachinery Technical Conference and Exposition . 2020

机译：在具有边界层摄取的跨音尾锥推进器风扇阶段调查入口失真的不稳定方法
5. Analysis of Inlet Distortion Patterns on Distortion Transfer and Generation Through a Highly Loaded Fan Stage [D] . ?Orme, Andrew Dallin 2020

机译：在失真传递和代进气畸变模式的分析通过高负荷风扇级
6. Effect of Inlet Air Volumetric Flow Rate on the Performanceof a Two-Stage Cyclone Separator [O] . Jihe Chen, Zhong-an Jiang, *, 2018

机译：进气量流量对性能的影响二级旋风分离器
7. Discussion: “An Experiment With Aspect Ratio as a Means of Extending the Useful Range of a Transonic Inlet Stage of an Axial Flow Compressor” (Swan, W. C., 1964, ASME J. Eng. Power, 86, pp. 243–246) [O] . W. K. Bodger 1965

机译：讨论：“具有纵横比的实验，作为延长轴流压缩机的跨音进气级的有用范围的手段”（Swan，W.C.，1964，Asme J. Eng。Power，86，PP。243-246）

Undistorted inlet flow testing. Evaluation of range and distortion tolerance for high Mach number transonic fan stages, volume 2 Task 2 stage data and performance report

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