[1] 李倩, 洪延姬, 叶继飞, 等. LSDW速度随激光参数和环境气体压强变化规律的实验研究[J]. 推进技术, 2010, 31(1): 123-128. (LI Qian, HONG Yan-ji, YE Ji-fei, et al. Experimental Study on Effects of Laser Parameters and Ambient Air Pressure on LSDW Velocity[J]. Journal of Propulsion Technology, 2010, 31(1): 123-128.)
[2] 李倩, 金星, 曹正蕊, 等. 激光等离子体点源减阻技术中入射能量对气动阻力的影响[J]. 推进技术, 2010, 31(3): 377-380. (LI Qian, JIN Xing, CAO Zheng-rui, et al. Effects on Aerodynamic Drag of Incident Laser Energy in Technology of Laser Plasma Point Source Drag Reduction[J]. Journal of Propulsion Technology, 2010, 31(3): 377-380.)
[3] Adelgren R, Elliott G, Knight D, et al. Energy Deposition in Supersonic Flows[R]. AIAA 2001-0885.
[4] Erinc Erdem, Leichao Yang, Konstantinos Kontis. Drag Reduction Studies by Steady Energy Deposition at Mach 5[R]. AIAA 2011-1027.
[5] Kim J H, Matsuda A, Sakai T, et al. Drag Reduction with High-Frequency Repetitive Side-on Laser Pulse Energy Depositions[R]. AIAA 2010-5104.
[6] Myrabo L N, Raizer Yu P, Shneider M N. Drag and Total Power Reduction for Artificial Heat Input in Front of Hypersonic Blunt Body[R]. Beamed Energy Propulsion: Third International Symposium on Beamed Energy Propulsion, 2005: 485-498.
[7] Riggins D, Nelson H F, Johnson E. Blunt-Body Wave Drag Reduction Using Focused Energy Deposition[J]. AIAA Journal, 1999, 37(4): 460-467.
[8] David Sperber, Fabian Schmid, Hans-Albert Eckel, et al. Wave Drag Reduction of Blunt Bodies Using Laser Sustained Energy Deposition in Argon Atmosphere[R]. AIAA 2012-2815.
[9] Taylor T. Drag Reduction and Control Using Energetic and Electrostatic Force-Fields for Hypersonic Applications[R]. AIAA 2004-0131.
[10] Ogino Y, Ohnishi N, Taguchi S H, et al. Baroclinic Vortex Influence on Wave Drag Reduction Induced by Pulse Energy Deposition[J]. Physics of Fluids, 2009, 21(6).
[11] Hong Yanji, Wang Diankai, Li Qian, et al. Interaction of Single-Pulse Laser Energy with Bow Shock in a Hypersonic Flow[J]. Chinese Journal of Aeronautics, 2014, 27(2): 241-247.
[12] 方娟, 洪延姬, 李倩, 等. 高重复频率激光能量沉积减小超声速波阻的数值研究[J]. 强激光与粒子束, 2011, 23(5): 1158-1162.
[13] Skvotrsov V, Kuznetsov Yu. Consequences of Heat Concept of Electrical Discharge Influence on Aerodynamic Characteristics for Comparative Experiments in Aerodynamics[R]. AIAA 2001-3051.
[14] 方娟. 激光“空气锥”减小超声速飞行器波阻的方法研究[D]. 北京:装备学院, 2012: 87-112.
[15] 王殿恺. 光能量控制高超声速波系结构特性研究[D]. 北京:装备学院, 2013: 34-41. * 收稿日期:2016-01-08;修订日期:2016-03-04。基金项目:国家自然科学基金项目(11372356);国家重点实验室自主研究课题。作者简介:王殿恺,男,博士,助理研究员,研究领域为等离子体流动控制。E-mail: diankai@mail.ustc.edu.cn(编辑:梅瑛)
|