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作 者:NIE ChaoQun LI Gang ZHU JunQiang ZHANG Yi LI YuTong
机构地区:[1]Key Laboratory of Advanced Energy and Power of Chinese Academy of Sciences at Institute of Engineering Thermophysics,Beijing 100080,China [2]Laboratory of Optical Physics,Institute of Physics,Chinese Academy of Sciences,Beijing 100080,China
出 处:《Science China(Technological Sciences)》2008年第7期1064-1072,共9页中国科学(技术科学英文版)
基 金:the National Natural Science Foundation of China (Grant Nos. 50406027, 50676094)
摘 要:Effects of plasma flow control are researched on the basis of plasma exciting flow experiments and numerical simulations. Turbulent model is more effective than laminar model in plasma numerical simulation as results showed. Both plasma exciting effects of acceleration and flow separation suppression are investigated through experiments carried on the flat plate and the compressor cascades. The results demonstrate that boundary layer characteristic is modified by plasma exciting. Distributions of total pressure and velocity in the wake are improved notably for 20 m/s coming velocity and the effect of plasma can still be observed while velocity is increased to 50 m/s. For low velocity flow, plasma exciting is effective in flow separation suppression.Effects of plasma flow control are researched on the basis of plasma exciting flow experiments and numerical simulations. Turbulent model is more effective than laminar model in plasma numerical simulation as results showed. Both plasma exciting effects of acceleration and flow separation suppression are investigated through experiments carried on the flat plate and the compressor cascades. The results demonstrate that boundary layer characteristic is modified by plasma exciting. Distributions of total pressure and velocity in the wake are improved notably for 20 m/s coming velocity and the effect of plasma can still be observed while velocity is increased to 50 m/s. For low velocity flow, plasma exciting is effective in flow separation suppression.
关 键 词:FLOW control dielectric barrier discharge PLASMA PLASMA EXCITING COMPRESSOR CASCADE FLOW separation
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