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The thrust of ionic wind exciters in 19 points-grid and 31 points-grid electrodes configurations was measured in this paper by means of air suspension test platform without friction. Meanwhile, a control method was also provided for multipoint-grid ionic wind exciter. And then the study was done on the factors, e.g. the gap of point-grid electrodes, the spacing between points, the curvature radius of the point, and the voltage, current of corona discharge, all of which may affect the thrust character; so some methods for getting high thrust at low power were also proposed in order to improve the thrust and the thrust per unit power at the same time.
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Keywords:
- ionic wind /
- multipoint-grid electrodes /
- thrust /
- ratio of thrust and power
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[2] Go D B, Garimella S V, Fisher T S 2007 J. Appl. Phys. 102 1
[3] Moreau E 2007 J. Phys. D: Appl. Phys. 40 605
[4] Chen Y H, Barthakur N N 1991 Int. J. Biometeorol. 35 67
[5] Moreau E, Touchard G 2008 J. Electrostat 66 39
[6] Rickard M, Dunn-Rankin D, Weinberg F, Carleton F 2006 J. Electrostat 64 368
[7] Takeuchi N, Yasuoka K 2009 IEEE Trans. Plasma Sci. 37 1021
[8] Qiu W, Xia L Z, Yang L J 2010 IEEE Trans. Plasma Sci. 38 2848
[9] Porter C O, Baughn J W, McLaughlin T E, Enloe C L, Font G I 2007 AIAA 45 1562
[10] Wilson J, Perkins H D, Thompson W K 2009
[11] Pekkerd L, Young M 2011 J. Propul. Power 27 786
[12] Zhang G Q, Ge Y J, Zhang Y F, Chen G L 2004 Chin. Phys. Lett. 21 2238
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[14] Feng S, He F, Oyang J T 2007 Chin. Phys. Lett. 24 2304
[15] Akbar D, Bilikmen S 2006 Chin. Phys. Lett. 23 1234
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[17] Dong L F, Wang L, Li X C 2005 Chin. Phys. 14 1418
[18] Thierry C, Jean-Pierre B, Ouyang J T, Cao J 2004 Chin. Phys. 13 1907
[19] Li S, Ouyang J T, He F 2010 Chin. Phys. Lett. 27 065201
[20] Chen G L , Fan S H , Li C L 2005 Chin. Phys. Lett. 22 1980
[21] Li X C, Yuan N, Jia P Y, Chang Y Y, Ji Y F 2011 Acta Phys. Sin. 60 3324 (in Chinese) [李雪辰, 袁宁, 贾鹏英, 常媛媛, 嵇亚飞 2011 60 125204]
[22] Zhang Z H, Shao X J, Zhang G J, Li Y X, Peng Z Y 2012 Acta Phys. Sin. 61 3324 (in Chinese) [张增辉, 邵先军, 张冠军, 李娅西, 彭兆裕 2012 61 045205]
[23] Shao X J, Ma Y, Li Y X, Zhang G J 2010 Acta Phys. Sin. 59 8747 (in Chinese) [邵先军, 马跃, 李娅西, 张冠军 2010 59 8747]
[24] Hao Y P, Yang L, Tu E L, Chen J Y, Zhu Z W, Wang X L 2010 Acta Phys. Sin. 59 2610 (in Chinese) [郝艳捧, 阳林, 涂恩来, 陈建阳, 朱展文, 王晓著 2010 59 2610]
[25] Yu Z, Zhang Z T, Yu Q X, Xu S J, Yao J, Bai M D, Tian Y P, Liu K Y 2012 Acta Phys. Sin. 61 195202 (in Chinese) [俞哲, 张芝涛, 于清旋, 许少杰, 姚京, 白敏冬, 田一平, 刘开颖 2012 61 195202]
[26] Wei H L, Liu Z L, Li Z G, Zheng Q G 1996 Chin. Phys. 15 520
[27] Ren J X, Liu Y, Jiang X L, Le X Y, Wang L Y 2010 J. Aerospace Power 25 1395 (in Chinese) [任军学, 刘宇, 江兴流, 乐晓云, 王立英 2010 航空动力学报 25 1395]
[28] Jaworek A, Krupa A 1995 Czech J. Phys. 45 1035
[29] Metwally I A 1996 IEEE Trans. Dielect. El. In. 3 544
[30] Lacoste D A, Pai D, Laux C O 2004 42nd AIAA Aerospace Sciences Meeting and Exhibit Reno, Nevada, January 5–8, 2004
[31] Micci M M, Ketsdever A D 2000 Micropropulsion for Small Spacecraft AIAA p211
[32] Polzin K A, Markusic T E, Stanojev B 2006 J. Am. In. Phys. 77 105108
[33] Murakami H 1984 J. Spacecraft 21 96
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[1] Robinson M 1961 AIEE Trans 80 143
[2] Go D B, Garimella S V, Fisher T S 2007 J. Appl. Phys. 102 1
[3] Moreau E 2007 J. Phys. D: Appl. Phys. 40 605
[4] Chen Y H, Barthakur N N 1991 Int. J. Biometeorol. 35 67
[5] Moreau E, Touchard G 2008 J. Electrostat 66 39
[6] Rickard M, Dunn-Rankin D, Weinberg F, Carleton F 2006 J. Electrostat 64 368
[7] Takeuchi N, Yasuoka K 2009 IEEE Trans. Plasma Sci. 37 1021
[8] Qiu W, Xia L Z, Yang L J 2010 IEEE Trans. Plasma Sci. 38 2848
[9] Porter C O, Baughn J W, McLaughlin T E, Enloe C L, Font G I 2007 AIAA 45 1562
[10] Wilson J, Perkins H D, Thompson W K 2009
[11] Pekkerd L, Young M 2011 J. Propul. Power 27 786
[12] Zhang G Q, Ge Y J, Zhang Y F, Chen G L 2004 Chin. Phys. Lett. 21 2238
[13] Jiang N, Cao Z X 2010 Acta Phys. Sin. 59 3324 (in Chinese) [江南, 曹则贤 2010 59 3324]
[14] Feng S, He F, Oyang J T 2007 Chin. Phys. Lett. 24 2304
[15] Akbar D, Bilikmen S 2006 Chin. Phys. Lett. 23 1234
[16] Wang D Z, Wu H T 2002 Chin. Phys. 11 799
[17] Dong L F, Wang L, Li X C 2005 Chin. Phys. 14 1418
[18] Thierry C, Jean-Pierre B, Ouyang J T, Cao J 2004 Chin. Phys. 13 1907
[19] Li S, Ouyang J T, He F 2010 Chin. Phys. Lett. 27 065201
[20] Chen G L , Fan S H , Li C L 2005 Chin. Phys. Lett. 22 1980
[21] Li X C, Yuan N, Jia P Y, Chang Y Y, Ji Y F 2011 Acta Phys. Sin. 60 3324 (in Chinese) [李雪辰, 袁宁, 贾鹏英, 常媛媛, 嵇亚飞 2011 60 125204]
[22] Zhang Z H, Shao X J, Zhang G J, Li Y X, Peng Z Y 2012 Acta Phys. Sin. 61 3324 (in Chinese) [张增辉, 邵先军, 张冠军, 李娅西, 彭兆裕 2012 61 045205]
[23] Shao X J, Ma Y, Li Y X, Zhang G J 2010 Acta Phys. Sin. 59 8747 (in Chinese) [邵先军, 马跃, 李娅西, 张冠军 2010 59 8747]
[24] Hao Y P, Yang L, Tu E L, Chen J Y, Zhu Z W, Wang X L 2010 Acta Phys. Sin. 59 2610 (in Chinese) [郝艳捧, 阳林, 涂恩来, 陈建阳, 朱展文, 王晓著 2010 59 2610]
[25] Yu Z, Zhang Z T, Yu Q X, Xu S J, Yao J, Bai M D, Tian Y P, Liu K Y 2012 Acta Phys. Sin. 61 195202 (in Chinese) [俞哲, 张芝涛, 于清旋, 许少杰, 姚京, 白敏冬, 田一平, 刘开颖 2012 61 195202]
[26] Wei H L, Liu Z L, Li Z G, Zheng Q G 1996 Chin. Phys. 15 520
[27] Ren J X, Liu Y, Jiang X L, Le X Y, Wang L Y 2010 J. Aerospace Power 25 1395 (in Chinese) [任军学, 刘宇, 江兴流, 乐晓云, 王立英 2010 航空动力学报 25 1395]
[28] Jaworek A, Krupa A 1995 Czech J. Phys. 45 1035
[29] Metwally I A 1996 IEEE Trans. Dielect. El. In. 3 544
[30] Lacoste D A, Pai D, Laux C O 2004 42nd AIAA Aerospace Sciences Meeting and Exhibit Reno, Nevada, January 5–8, 2004
[31] Micci M M, Ketsdever A D 2000 Micropropulsion for Small Spacecraft AIAA p211
[32] Polzin K A, Markusic T E, Stanojev B 2006 J. Am. In. Phys. 77 105108
[33] Murakami H 1984 J. Spacecraft 21 96
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