Art

J-GLOBAL ID：202002217307060527   Reference number：20A1160039

Development of DC Discharge Power Supply System and Its Performance Test for the Experiment of the Interaction between the Shock Wave and the Discharge Plasma

衝撃波と放電プラズマの干渉実験用直流放電装置試作及び性能確認実験

Author (9)： MATSUDA ATSUSHI (名城大学) ,  OKADA KENJI (名城大学) ,  OKADA KENJI (現 日鉄テックスエンジ) ,  KOIZUMI SHINJI (名城大学) ,  KOIZUMI SHINJI (現 デンソーテクノ) ,  AOYAMA NAOKI (名城大学) ,  AOYAMA NAOKI (現 東芝) ,  KITO TAKUHIRO (名城大学) ,  KITO TAKUHIRO (現 日軽エムシーアルミ)
Material： 航空宇宙技術(Web)  (Aerospace Technology Japan, the Japan Society for Aeronautical and Space Sciences (Web))
Volume： 19  Page： 57-62(J-STAGE)  Publication year： 2020 
JST Material Number： U0120A  ISSN： 1884-0477  Document type： Article
Article type： 原著論文  Country of issue： Japan (JPN)  Language： JAPANESE (JA)

Thesaurus term： shock wave ,  plasma ,  *interferometry ,  *DC power source ,  *plasma production ,  performance evaluation ,  *shock tube ,  flow field ,  spectroscopy ,  *supersonic aircraft ,  aerodynamic characteristic
Semi thesaurus term： *discharge plasma ,  干渉実験 ,  放電装置 ,  spectrometry

Author keywords (6)： DC Discharge ,  DC Discharge Plasma ,  Interaction between the Shock Wave and the Plasma ,  DC Discharge ,  DC Discharge Plasma ,  Interaction between the Shock Wave and the Plasma

JST classification (2)： Aerodynamics of aircrafts  (QK02010T) ,  High-speed aerodynamics  (BC03000C)

Reference (20)：

• 1) Tret'yakov, P. K., Garanin, A. F., Grachev, G. N., Krainev, V. L., Ponomarenko, A. G., Tishchenko, V. N., Yakovlev, V. I., and Chernyi, G. G.: Control of Supersonic Flow Around Bodies by Means of High-power Recurrent Optical Breakdown, Physics - Doklady, 41 (1996), pp. 566-567.\n
• 2) Sasoh, A., Sekiya, Y., Sakai, T., Kim, J.-H., and Matsuda, A.: Supersonic Drag Reduction with Repetitive Laser Pulses Through a Blunt Body, AIAA Journal, 48 (2010), pp. 2811-2817.
• 3) Adelgren, R. G., Yan, H., Elliott, G. S., Knight, D. D., Beutner, T. J., and Zheltovodov, A. A.: Control of Edney IV Interaction by Pulsed Laser Energy Deposition, AIAA Journal, 43 (2005), pp. 256-269.
• 4) Knight, D. D.: Survey of Aerodynamic Drag Reduction at High Speed by Energy Deposition, Journal of Propulsion and Power, 24 (2008), pp. 1153-1167.
• 5) Erdem, E., Kontis, K., and Yang, L.: Steady Energy Deposition at Mach 5 for Drag Reduction, Shock Waves, 23 (2013), pp. 285-289

Terms in the title (7)： 衝撃波 ,  放電プラズマ ,  干渉 ,  実験 ,  直流 ,  試作 ,  確認実験