Volume 34 Issue 3
May  2014
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Cai Honghua, Nie Wansheng, Feng Songjiang. Analysis of Surface Wave Plasma Drag Reduction Properties in Near Space[J]. Chinese Journal of Space Science, 2014, 34(3): 304-312. doi: 10.11728/cjss2014.03.304
Citation: Cai Honghua, Nie Wansheng, Feng Songjiang. Analysis of Surface Wave Plasma Drag Reduction Properties in Near Space[J]. Chinese Journal of Space Science, 2014, 34(3): 304-312. doi: 10.11728/cjss2014.03.304

Analysis of Surface Wave Plasma Drag Reduction Properties in Near Space

doi: 10.11728/cjss2014.03.304
  • Received Date: 2013-08-11
  • Rev Recd Date: 2013-10-29
  • Publish Date: 2014-05-15
  • In order to investigate the drag reduction effect of surface wave plasma in near space, this paper analyzes the surface wave plasma flow control mechanism based on basic characteristics of the fluid control macro model, simulates its flow field in the 0 degree angle of attack based on the airship model. The drag reduction effect of different actuator control program is compared, and the plasma flow control effect on the airship tail is studied. Results show that the surface wave plasma can increase the airship lift and reduce its flight resistance. The airship lift can be increased through the unilateral control scheme, while the symmetrical control scheme is invalid for the airship lift because of the airship force balance in the vertical direction. The maximum drag reduction effect of unilateral control scheme is about 7 percent, and the symmetrical control scheme is better than unilateral one with its maximum drag reduction effect up to about 32 percent. The surface wave plasma has good elimination and inhibition of flow separation in the airship tail.

     

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  • [1]
    Liu Jun. Overseas slow near space vehicles and technological development (next)[J]. Aerosp. China, 2012, 1:31-35. In Chinese (刘军. 国外低速临近空间飞行 器与技术发展(下)[J]. 中国航天, 2012, 1:31-35)
    [2]
    Ji Yan. The development overview of overseas near space vehicle technology[J]. Int. Aviat., 2006, 9:84-85. In Chinese (季艳. 国外临近空间飞行器技 术发展概述[J]. 国际航空, 2006, 9:84-85)
    [3]
    Xu Li, Zhang Qiuping. Research trends of overseas near space vehicles[J]. Elect. Eng., 2011, 2:52-57. In Chinese (徐莉, 张秋萍. 国外临近空间飞行器研究动态[J]. 电子工程, 2011, 2:52-57)
    [4]
    Li Yiyong, Li Zhi, Shen Huairong. Analysis on development and application of near space vehicle[J]. J. Acad. Equip. Com. Tech., 2008, 19:61-65. In Chinese (李怡勇, 李智, 沈怀荣. 临近空间飞行器发展与应用分析[J]. 装备指 挥技术学院学报, 2008, 19(2):61-65)
    [5]
    Yang Bo, Bai Mindi, Xue Xiaohong, et al. Recent progress in plasma flow control[J]. Sci. Tech. Rev., 2009, 24:81-85. In Chinese (杨波, 白敏菂, 薛晓红, 等. 等离子体流动控制研究进展[J]. 科技导报, 2009, 24:81-85)
    [6]
    Dong Taiyuan, Ye Kuntao, Liu Weiqing. The current status of surface wave plasma source development[J]. Acta Phys. Sin., 2012, 61(14):145202. In Chinese (董太源, 叶坤涛, 刘维清. 表面波等离子体源的发展现状[J]. 物理 学报, 2012, 61(14):145202)
    [7]
    Cheng Yufeng, Nie Wansheng, Che Xueke. Numerical analysis of dielectric barrier discharge plasma aerodynamic actuation in near space[J]. High Volt. Eng., 2011, 37:1542-1547. In Chinese (程钰锋, 聂万胜, 车学科. 临近空间介质阻挡放电等离子体气动激励效果的数 值分析[J]. 高电压技术, 2011, 37:1542-1547)
    [8]
    Cheng Yufeng, Nie Wansheng, Li Guoqiang. Numerical study of plasma aerodynamic actuation mechanism[J]. Acta Phys. Sin., 2012, 61(6):95-103. In Chinese (程钰锋, 聂万胜, 李国强. 等离子体气动激励机理数值研究[J]. 物 理学报, 2011, 61:060509)
    [9]
    Liu Minghai, Sugai H, Hu Xiwei, et al. Properties of large-area surface wave plasma[J]. Acta Phys. Sin., 2006, 55(11):5905-5908. In Chinese (刘明海, 菅井秀郞, 胡希伟, 等. 大面积表面波等离子体的特性研究[J]. 物理学报, 2006, 55(11):5905-5908)
    [10]
    Chen Zhaoquan, Liu Minghai, Lan Chaohui, et al. A numerical simulation of surface wave excitation in a rectangular planar-type plasma source[J]. Chin. Phys.: B, 2009, 18(8):3484-3489
    [11]
    Feng Songjiang, Cai Honghua, Tian Xihui, et al. Study of application of ambient plasma wave for near spaceairship drag-reduction[J]. J. Acad. Equip., 2013, 24(4):59-62. In Chinese (丰松江, 蔡红华, 田希晖, 等. 表面等离子体波在临近空间飞艇减阻中的应用研究[J]. 装备学院学报, 2013, 24(4):59-62)
    [12]
    Zhou Benmou, Fan Baochun, Chen Zhihua, et al. Experimental study on circular-cylinder flow modified by electromagnetic body forces[J]. Eng. Mech., 2006, 23(4):172-176. In Chinese (周本谋, 范宝春, 陈志华, 等. 电磁体积力作用下的圆柱绕流实验研究[J]. 工程力学, 2006, 23(4):172-176)
    [13]
    Liu Huixing, Zhou Benmou, Liu Zongkai, et al. Drag reduction of rudder controlled by spanwise electromagnetic force[J]. J. Hebei Univ.: (Nat. Sci.), 2010, 30(5):485-489. In Chinese (刘会星, 周本谋, 刘宗凯, 等. 展 向电磁力对舵面的湍流减阻控制[J]. 河北大学学报(自然科学版), 2010, 30(5):485-489)
    [14]
    Chen Raohui, Fan Baochun, Chen Zhihua, et al. Flow pattern and lift evolution of hydrofoil with control of electro-magnetic forces[J]. Sci. China Ser.: G, 2009, 39(8):1141-1150. In Chinese (陈耀慧, 范宝春, 陈志华, 等. 电磁力控制下的翼型绕流和升力[J]. 中国科学, 2009, 39(8):1141-1150)
    [15]
    Michael A L, Allan J L. Principles of Plasma Discharges and Materials Processing(2 ed)[M]. Beijing: Science Press, 2007:72-74. In Chinese (Michael A L, Allan J L. 等离子体放电原理与材料处理(第2版)[M]. 北京: 科学出版社, 2007: 72-74)
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