| 等离子体流动控制技术研究进展 |
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| 引用本文： | 李应红,吴云.等离子体流动控制技术研究进展[J].空军工程大学学报,2012(3):1-5. |
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| 作者姓名： | 李应红 吴云 |
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| 作者单位： | 空军工程大学等离子体动力学重点实验室 |
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| 基金项目： | 国家自然科学基金资助项目(10972236;50906100) |
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| 摘 要： | 基于等离子体气动激励的等离子体流动控制技术,可显著改善飞行器/动力装置的气动特性,已成为国际上空气动力学和气动热力学领域的研究前沿。简要介绍国外等离子体流动控制研究的重要进展,主要介绍国内在等离子体冲击波流动控制理论、等离子体气动激励特性、等离子体气动激励扩大压气机稳定性、等离子体气动激励减弱超/高超声速激波强度等方面的研究进展,并指出了未来发展需要解决的重大问题。
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| 关 键 词： | 等离子体 流动控制 等离子体气动激励 压气机 |
Progress of Research on Plasma Flow Control Technology |
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| LI Ying-hong,WU Yun.Progress of Research on Plasma Flow Control Technology[J].Journal of Air Force Engineering University(Natural Science Edition),2012(3):1-5. |
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| Authors: | LI Ying-hong WU Yun |
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| Institution: | (Science and Technology on Plasma Dynamics Lab,Air Force Engineering University,Xi′an 710038,China) |
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| Abstract: | Plasma flow control can significantly improve the aerodynamic characteristics of aircraft and power plant through plasma aerodynamic actuation,and this technology has already become a front subject in international aerodynamics and aerothermodynamics fields.Status of overseas plasma flow control research is introduced briefly.Progress of Air Force Engineering University in plasma shock flow control theory,plasma aerodynamic actuation characteristics,plasma based compressor stability extension and shock control is presented.Also,the important problems in future are pointed out. |
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| Keywords: | plasma flow control plasma aerodynamic actuation compressor |
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