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螺旋桨等离子体流动控制的增效实验

陈庆亚 田希晖 姜家文 聂万胜 车学科

陈庆亚, 田希晖, 姜家文, 聂万胜, 车学科. 螺旋桨等离子体流动控制的增效实验[J]. 航空动力学报, 2016, 31(5): 1205-1211. doi: 10.13224/j.cnki.jasp.2016.05.023
引用本文: 陈庆亚, 田希晖, 姜家文, 聂万胜, 车学科. 螺旋桨等离子体流动控制的增效实验[J]. 航空动力学报, 2016, 31(5): 1205-1211. doi: 10.13224/j.cnki.jasp.2016.05.023
CHEN Qing-ya, TIAN Xi-hui, JIANG Jia-wen, NIE Wan-sheng, CHE Xue-ke. Experiment on the performance of propeller plasma flow control[J]. Journal of Aerospace Power, 2016, 31(5): 1205-1211. doi: 10.13224/j.cnki.jasp.2016.05.023
Citation: CHEN Qing-ya, TIAN Xi-hui, JIANG Jia-wen, NIE Wan-sheng, CHE Xue-ke. Experiment on the performance of propeller plasma flow control[J]. Journal of Aerospace Power, 2016, 31(5): 1205-1211. doi: 10.13224/j.cnki.jasp.2016.05.023

螺旋桨等离子体流动控制的增效实验

doi: 10.13224/j.cnki.jasp.2016.05.023
基金项目: 

高分专项青年创新基金(GFZX04060103-5)

国家自然科学基金(11205244)

详细信息
    作者简介:

    陈庆亚(1991-),男,河北沧州人,硕士生,主要从事等离子体流动控制技术.

  • 中图分类号: V211.44

Experiment on the performance of propeller plasma flow control

  • 摘要: 实验依托搭建的螺旋桨等离子体流动控制测试平台,基于等离子体附壁射流抑制边界层分离的两种机制,采用等离子体射流与来流方向相同的正向射流方式和与来流方向相反的逆向射流方式,研究了微秒脉冲等离子体射流对螺旋桨三维流动分离的控制效果,对比分析了两种射流方式增效特点.实验结果表明:在螺旋桨转速为300r/min,电压峰值为8.5kV,脉冲频率为10~160Hz范围内,正向射流有利于减小螺旋桨转矩,逆向射流对转矩的效果则相反.两种射流方式均提高了螺旋桨拉力和效率,同时其控制效果受脉冲频率的影响较大;正向和逆向两种射流分别使螺旋桨效率最大提高了11.56%,2.79%.

     

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出版历程
  • 收稿日期:  2015-04-23
  • 刊出日期:  2016-05-28

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