| 李应红，吴云，宋慧敏，张朴，魏沣亭.大气压等离子体流动控制实验[J].空军工程大学学报,2006,(3):1-3 |
| 大气压等离子体流动控制实验 |
| Preliminary Experimental Investigation of Atmosphere Plasma Flow Control Technology |
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| DOI： |
| 中文关键词: 航空、航天推进系统 大气压等离子体 流动控制 放电 实验 |
| 英文关键词: aerospace propulsion system atmosphere plasma flow control discharge experiment |
| 基金项目:国家“863”计划资助项目（2003AA753025） |
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| 摘要点击次数: 3509 |
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| 中文摘要: |
| 进行了大气压等离子体流动控制初步实验。在等离子体激励器表面产生了大气压等离子体，验证了不对称布局等离子体激励器诱导边界层加速的现象；发现了一个不对称布局的激励器和一个对称布局的激励器并联、垂直布置的情况下，不对称布局激励器表面边界层加速现象消失，对称布局激励器表面边界层发生了旋涡运动；验证了等离子体激励抑制翼型失速分离的有效性。 |
| 英文摘要: |
| Elementary atmosphere plasma flow control experiment is performed. Atmosphere plasma is generated on the surface of plasma actuator and the phenomenon of asymmetric plasma actuator inducing boundary layer to accelerate is verified. It is found that in the case of laying a symmetric actuator and an asymmetric actuator in bridge and vertically, the acceleration phenomenon of boundary layer on the surface of asymmetric actuator will disappear and a vortex motion of boundary layer on the surface of symmetric actuator will arise. The effectiveness of using plasma actuation to suppress airfoil stall separation is verified. |
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