不同激励模式的端壁脉冲吹气控制高负荷压气机叶栅流动分离

IF 0.7 4区 工程技术 Q4 ENGINEERING, AEROSPACE
Hongxin Zhang, Jian-Jun Ye, Bo Jin, C. Xu, Guoping Huang
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引用次数: 0

摘要

为了提高高负荷压气机的气动性能,研究了三种不同激励波形下的端壁脉冲吹气。对激励频率和动量系数等重要激励参数进行了详细分析。并与端壁稳定吹气(ESB)情况进行了比较。对于具有三种激励波形(正弦、三角形和梯形波形)的epb,激励频率等于旋涡脱落固有频率的整数倍是最优的,并且比具有相同时间平均动量系数的ESB具有更好的性能。此外,三种激励波形的epb在气动性能改善方面存在显著差异。采用波形三角形的EPB实现了最佳工况,总压损失系数降低了25.64%。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Endwall-pulsed blowing of different excitation models to control flow separation on a highly-loaded compressor cascade
Abstract Endwall-pulsed blowing (EPB) is studied for three different excitation waveforms to improve the aerodynamic performance of highly loaded compressors. Some important excitation parameters include the excitation frequency and momentum coefficient, which were analyzed in detail. The results of the EPB are compared with the endwall steady blowing (ESB) case. For EPBs with the three excitation waveforms (Waveforms sine, triangle and trapezoid), excitation frequencies that are equal to an integral multiple of the natural frequency of the vortex shedding are optimal and provide better performances than the ESB with the same time-mean momentum coefficient. Moreover, the EPBs of the three excitation waveforms have significant differences in their aerodynamic performance improvements. The optimal case is achieved by the EPB with Waveform triangle and provides a total pressure loss coefficient with a reduction of 25.64%.
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来源期刊
International Journal of Turbo & Jet-Engines
International Journal of Turbo & Jet-Engines 工程技术-工程:宇航
CiteScore
1.90
自引率
11.10%
发文量
36
审稿时长
6 months
期刊介绍: The Main aim and scope of this Journal is to help improve each separate components R&D and superimpose separated results to get integrated systems by striving to reach the overall advanced design and benefits by integrating: (a) Physics, Aero, and Stealth Thermodynamics in simulations by flying unmanned or manned prototypes supported by integrated Computer Simulations based on: (b) Component R&D of: (i) Turbo and Jet-Engines, (ii) Airframe, (iii) Helmet-Aiming-Systems and Ammunition based on: (c) Anticipated New Programs Missions based on (d) IMPROVED RELIABILITY, DURABILITY, ECONOMICS, TACTICS, STRATEGIES and EDUCATION in both the civil and military domains of Turbo and Jet Engines. The International Journal of Turbo & Jet Engines is devoted to cutting edge research in theory and design of propagation of jet aircraft. It serves as an international publication organ for new ideas, insights and results from industry and academic research on thermodynamics, combustion, behavior of related materials at high temperatures, turbine and engine design, thrust vectoring and flight control as well as energy and environmental issues.
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