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Aerodynamic Performance of an Over-the-Rotor Liner with Circumferential Grooves on a High Bypass Ratio Turbofan Rotor.

机译：高旁通比涡扇转子上具有圆周槽的转子衬套的空气动力学性能。

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作者
Bozak, R.; Hughes, C.; Buckley, J.;
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年度 2013
页码 1-19
总页数 19
原文格式 PDF
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Aerodynamic characteristics; Linings; Circumferences; Grooves; Bypass ratio; Turbofans; Rotors; Aeroacoustics; Wind tunnel tests; Noise reduction; Static tests; Engine tests; Metal foams; Error analysis; Pressure ratio; Temperature ratio; Adiabatic conditions;

机译：空气动力学特性;衬里;圆周;凹槽;旁通比;涡轮风扇;转子;气动声学;风洞试验;降噪;静态试验;发动机试验;金属泡沫;误差分析;压力比;温度比;绝热条件;

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1. High-Speed Turbofan Noise Reduction Using Foam-Metal Liner Over-the-Rotor [J] . Daniel L. Sutliff, Michael G. Jones, Thomas C. Hartley Journal of Aircraft . 2013,第5期

机译：泡沫金属衬套在转子上的高速涡轮风扇降噪
2. Aerodynamic design of an ultra-highly loaded booster of a high bypass ratio turbofan [J] . Chen Yuwen, Zhou Zhenggui, Cui Cui Proceedings of the Institution of Mechanical Engineers . 2019,第1期

机译：高旁路比涡轮风扇超高负荷增压器的空气动力学设计
3. INFLUENCE OF HIGH-BYPASS-RATIO TURBOFAN JETS ON AERODYNAMIC CHARACTERISTICS OF HIGH-LIFT WING [J] . A. V. Petrov, V.F. Tretyakov TsAGI science journal . 2015,第7期

机译：高旁路比涡轮风扇对高提升机翼气动特性的影响
4. THE AERODYNAMIC PERFORMANCE OF AN OVER-THE-ROTOR LINER WITH CIRCUMFERENTIAL GROOVES ON A HIGH BYPASS RATIO TURBOFAN ROTOR [C] . Rick Bozak, Christopher Hughes, James Buckley ASME turbo expo: turbine technical conference and exposition . 2013

机译：高旁路比涡轮风扇转子上带有圆周槽的衬套的气动性能
5. The Supersonic Performance of High Bypass Ratio Turbofan Engines with Fixed Conical Spike Inlets [D] . Cleary, Spencer. 2018

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6. Investigation of Penetration Performance of Zr-based Amorphous Alloy Liner Compared with Copper [O] . Ping Cui, Deshi Wang, Dongmei Shi, 2020

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7. Attenuation of FJ44 Turbofan Engine Noise with a Foam-Metal Liner Installed Over-the-Rotor [O] . Elliott Dave M., Hartley Thomas C., Sutliff Daniel L., 2009

机译：装有泡沫金属衬套的FJ44涡扇发动机的噪声降低
8. Aerodynamic Performance of an Over-the-Rotor Liner With Circumferential Grooves on a High Bypass Ratio Turbofan Rotor. [R] . C. E. Hughes J. Buckley R. F. Bozak 2013

机译：高旁通比涡扇转子上具有圆周槽的转子衬套的空气动力学性能。

Aerodynamic Performance of an Over-the-Rotor Liner with Circumferential Grooves on a High Bypass Ratio Turbofan Rotor.

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