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。
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 aero- dynamics and aerothermodynamics fields. Status of overseas plasma flow control research is introduced briefly. Pro- gress of Air Force Engineering University in plasma shock flow control theory, plasma aerodynamic actuation char- acteristics, plasma based compressor stability extension and shock control is presented. Also, the important prob- lems in future are pointed out.
出处
《空军工程大学学报（自然科学版）》
CSCD
北大核心
2012年第3期1-5,共5页
Journal of Air Force Engineering University(Natural Science Edition)
基金
国家自然科学基金资助项目(10972236
50906100)
