このリストは日本機械学会流体工学部門ニュースレター ながれ2007年12月号

DBDプラズマアクチュエータ -バリア放電を利用した新しい流体制御技術-

藤井孝藏（JAXA・ ISAS教授），松野隆（鳥取大・工学系研究科・講師）
の参考文献です

12/1/2007 JAXA宇宙科学研究本部 藤井研究室

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( 2) Shin, J., Narayanaswamy, V., Raja, L. L. and Clemens, N. T., Characteristics of a plasma actuator in Mach 3 flow, AIAA Paper 2007-788(2007).
( 3) Samimy, M., Kim, J.-H., Kastner, J., Adamovich, I. and Utkin, Y., Active Control of a Mach 0.9 Jet for Noise Mitigation Using Plasma Actuators, AIAA Journal 45(4):890-901
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( 4) Utkin, Y. G., Keshav, S., Kim, J.-H., Kastner, J., Adamovich, I. V. and Samimy, M., Characterization of Localized Arc Filament Plasma Actuators Used for High-speed Flow Control, AIAA Paper 2007-787(2007).
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( 7) Enloe, C. L., McLaughlin, T. E., VanDyken, R. D., Kachner, K. D., Jumper, E. J. and Corke, T. C., Mechanisms and Responses of a Single Dielectric Barrier Plasma Actuator: Plasma Morphology, AIAA Journal, Vol. 42, No.3 (2004), pp. 589-594.
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(12) Massines, F., Rabehi, A., Decomps, P., Ben Gadri, R., Segur, P. and Mayoux, C., Experimental and theoretical study of a glow discharge at atmospheric pressure controlled by dielectric barrier, Journal of Applied Physics, Vol. 83, No.6 (1998), pp. 2950-2957.
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(15) Font, G. I. and Morgan, W. L., Recent Progress in Dielectric Barrier Discharges for Aerodynamic Flow Control, Contrib. Plasma Phys., Vol. 47, No.1-2 (2007), pp. 103-110.
(16) Orlov, D. M., Apker, T., He, C., Othman, H. and Corke, T. C., Modeling and Experiment of Leading Edge Separation Control Using SDBD Plasma Actuators, AIAA Paper 2007-877(2007).
(17) Corke, T. C., Post, M. L. and Orlov, D. M., SDBD plasma enhanced aerodynamics: concepts, optimization and applications, Progress in Aerospace Sciences In Press, Corrected, Vol. Proof, No. (2007), pp. .
(18) Corke, T. C., Jumper, E. J., Post, M. L., Orlov, D. and McLaughlin, T. E., Application of weakly-ionized plasmas as wing flow-control devices, AIAA Paper 2002-350(2002).
(19) Post, M. L. and Corke, T. C., Separation Control on High Angle of Attack Airfoil Using Plasma Actuators, AIAA Journal, Vol. 42, No.11 (2004), pp. 2177-2184.
(20) Roth, J. R., Sherman, D. M. and Wilkinson, S. P., Electrohydrodynamic Flow Control with a Glow-Discharge Surface Plasma, AIAA Journal, Vol. 38, No.7 (2000), pp. 1166-1172.
(21) Post, M. L. and Corke, T. C., Separation Control Using Plasma Actuators: Dynamic Stall Vortex Control on Oscillating Airfoil, AIAA Journal, Vol. 44, No.12 (2006), pp. 3125-3135.
(22) Huang, J., Corke, T. C. and Thomas, F. O., Plasma Actuators for Separation Control of Low-Pressure Turbine Blades, AIAA Journal, Vol. 44, No.1 (2006), pp. 51-57.
(23) Huang, J., Corke, T. C. and Thomas, F. O., Unsteady Plasma Actuators for Separation Control of Low-Pressure Turbine Blades, AIAA Journal, Vol. 44, No.7 (2006), pp. 1477-1487.
(24) Van Ness II, D. K., Corke, T. C. and Morris, S. C., Stereo PIV of a Turbine Tip Clearance Flow with Plasma Actuation, AIAA Paper 2007-647(2007).
(25) Porter, C. O., McLaughlin, T. E., Enloe, C. L., Font, G. I., Roney, J. and Baughn, J. W., Boundary Layer Control Using a DBD Plasma Actuator, AIAA Paper 2007-786(2007).
(26) Nelson, R. C., Corke, T. C., He, C., Othman, H., Matsuno, T., Patel, M. P. and Ng, T. T., Modification of the Flow Structure over a UAV Wing for Roll Control, AIAA Paper 2007-884(2007).
(27) Lopera, J., Ng, T. T., Patel, M. P., Vasudevan, S. and Corke, T. C., Aerodynamic Control of 1303 UAV Using Windward Surface Plasma Actuators on a Separation Ramp, AIAA Paper 2007-636(2007).
(28) Chan, S., Zhang, X. and Gabriel, S., Attenuation of Low-Speed Flow-Induced Cavity Tones Using Plasma Actuators, AIAA Journal,, Vol. 45, No.7 (2007), pp. 1525-1538.
(29) Matsuno, T., Kawazoe, H., Nelson, R. C. and Corke, T. C., Active Control of Asymmetric Forebody Vortices Using Plasma Actuators, Proceedings of Third International Conference on Flow Dynamics, Tohoku University 21st COE program (2006), pp. 31-32.
(30) Matsuno, T., Kawazoe, H., and Nelson, R. C., Aerodynamic Control of High Performance Aircraft Using Plasma Actuators, Proceedings of the 2007 JSASS-KSAS Joint International Symposium on Aerospace Engineering(2007), pp. 44-47.
(31) 田中義輝, 藤井孝藏，プラズマアクチュエータによる火星航空機翼周り流れの制御，第19回数値流体力学シンポジウム講演論文集，B8-1 (2005).
(32) 椿野大輔, 田中義輝, 藤井孝藏，プラズマアクチュエータを用いた翼前縁剥離の制御における位置及び個数の影響，日本機械学会論文集B編, 第73巻727号, No. 06-0718 (2007), pp. 663-669.
(33) 田中元史，林和夫，松 田寿，大友文雄，野田悦夫，新関良樹，安井祐之，志村尚彦，藤井孝藏，大山聖，二宮由光，非平衡プラズマによる気流制御（第１報）−プラズマ誘起噴流による翼面剥離抑制効果―，第85期日本機会学会流体工学部門講演会講演論文集，503(2007).
(34) 松田寿，大友文雄，田中元史，林和夫，野田伸一，水野末良，内田竜朗，青木一義，新関良樹，野田悦夫，非平衡プラズマによる気流制御（第２報）−パルス変調制御の効果−，第85期日本機会学会流体工学部門講演会講演論文集，504(2007).
(35) 二宮由光，藤井孝藏，プラズマアクチュエータを用いた失速制御における周波数の影響，第45回飛行機シンポジウム講演集，1F1(2007)．
(36) 上田 忠雄,小河原 加久治, プラズマシンセティックジェットアクチュエータによる翼面はく離制御に関する数値実験, 第17 回数値流体力学シンポジウム講演論文, A4-2 (2003).
(37) Ogawara, K., Nakatani, N., Naka, T., Isobe, M. and Higuchi, T., Delayed Feedback Control for Flow around Wing using Plasma Synthetic Jet Actuator, AIAA Paper 2006-1406(2006).
(38) Abe, T., Takizawa, Y., Sato, S. and Kimura, N., A Parametric Experimental Study for Momentum Transfer by Plasma Actuator, AIAA Paper 2007-187(2007).
(39) Takizawa, Y., Matsuda, A., Kikuchi, K., Sasoh, A. and Abe, T., Optical Observation of Discharge Plasma Structure in DBD Plasma Actuator, AIAA Paper 2007-4376(2007).
(40) Segawa, T., Furutani, H., Yoshida, H., Jukes, T. and Choi, K.-S., Wall Normal Jet under Elevated Temperatures Produced by Surface Plasma Actuator, AIAA Paper 2007-784(2007).
(41) Isono, S., Takagaki, M., Nagai, H. and Asai, K., Investigation of the Plasma actuator performance on the Martian Atmosphere, Fourth International Conference on Flow Dynamics, Tohoku University 21st COE program 3-2-3(2007).
(42) 松野 隆，川添 博光，石田 誉, プラズマアクチュエータによる衝撃波位置制御の試み, 第39回流体力学講演会/航空宇宙シミュレーション技術シンポジウム2007講演論文集, (2007).