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Experimental investigation of an axial flow compressor inlet stage operating at transonic relative inlet Mach numbers I : over-all performance of stage with transonic rotor and subsonic stators up to rotor relative inlet Mach number of 1.1

机译：在跨音速相对入口马赫数下运行的轴流压气机进气级的实验研究I：跨音速转子和亚音速定子的级全部性能直到转子相对入口马赫数1.1

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Lieblein, Seymour; Lewis, George W , Jr; Sandercock, Donald M;
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年度 1952
页码 1-24
总页数 24
原文格式 PDF
正文语种 eng
中图分类工业技术;
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2. CFD ANALYSIS TO INVESTIGATE THE EFFECT OF LEANED ROTOR ON THE PERFORMANCE OF TRANSONIC AXIAL FLOW COMPRESSOR STAGE [J] . Akash M, M.T. Shobhavathy, R. Ajith Kumar Journal of Aerospace Sciences and Technologies . 2019,第1期

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3. 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

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4. EXPERIMENTAL AND NUMERICAL PERFORMANCE CHARACTERIZATION OF A TRANSONIC COMPRESSOR ROTOR OPERATING BEHIND AN INLET-GUIDE VANE WITH VARIABLE FLAP ANGLES [C] . Garth V. Hobson, Anthony Gannon, Wendell Holmes, ASME turbo expo: turbine technical conference and exposition . 2014

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5. Influence of axial spacing on spanwise efficiency of a transonic axial compressor rotor stage. [D] . Davey, Mark Willis. 2004

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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. Experimental noise studies of inlet-guide- vane-rotor-stator interactions for a single- stage axial-flow compressor [O] . Crigler, J. L., Copeland, W. L. 1965

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Experimental investigation of an axial flow compressor inlet stage operating at transonic relative inlet Mach numbers I : over-all performance of stage with transonic rotor and subsonic stators up to rotor relative inlet Mach number of 1.1

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