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单脉冲激光能量沉积对超声速钝头体波阻的影响 被引量:2

Effect of single pulse laser energy deposition on wave drag of supersonic flow blunt bodies
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摘要 采用数值模拟和实验手段对单脉冲条件下的激光能量沉积减小超声速钝头体波阻进行了系统地研究。首先利用数值仿真的方法模拟了马赫5的超声速气流条件下,能量沉积对半球体阻力特性的影响,通过压力温度等值线及驻点参数的变化规律,分析了能量沉积减阻机理。研究结果表明由于能量的注入,钝头体前弓形激波发生变形,激波脱体距离增大,降低了钝头体表面的压力,从而减小了钝头体的波阻,在单脉冲作用时间内,波阻减小了13%。建立了超声速条件下单脉冲激光能量沉积减阻实验系统,利用高分辨率的纹影系统拍摄激光能量沉积产生的激波与弓形激波相互作用过程,实验结果与数值模拟结果基本吻合。 Both numerical simulation and experiment are used to research the effect of single pulse laser energy deposition on supersonic wave drag.First,under the supersonic flow of Ma 5,the effect of energy deposition on wave drag is investigated with numerical simulation.The reason of drag reduction is analyzed by the law of the pressure,temperature contours and the parameter change of stagnation point.The results show that the bow shock over blunt body is deformed due to the energy deposition.The shock stand-off distance is increased,the surface pressure of blunt body is decreased and the wave drag is reduced by 13%.The experimental system is set up,and the interaction of shock and bow shock over the blunt body is screened by the schlieren system.The results of experiment and simulation are almost consistent.
出处 《光电子.激光》 EI CAS CSCD 北大核心 2012年第6期1057-1062,共6页 Journal of Optoelectronics·Laser
基金 国家自然科学基金(90916015)资助项目
关键词 激光 减阻 能量沉积 超声速气流 laser drag reduction energy deposition supersonic flow
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  • 1金星,洪延姬,崔村燕,王军,文明.激光推进冲量耦合系数的测量方法[J].强激光与粒子束,2004,16(7):861-864. 被引量:28
  • 2李修乾,洪延姬,何国强,姚宏林.激光推进器概念设计研究现状及发展趋势[J].强激光与粒子束,2005,17(3):363-368. 被引量:14
  • 3李倩,洪延姬,曹正蕊.吸气式激光推进推力产生机理的数值模拟[J].爆炸与冲击,2006,26(6):550-555. 被引量:25
  • 4Bushnell, D.M.: Shock wave drag reduction. Annu. Rev. Fluid. Mech. 36, 81-96 (2004).
  • 5Crawford, D.H.: Investigation of the flow over a spiked-nose hemisphere-cylinder at a Mach number of 6.8. NASA TN-D118 (1959).
  • 6Hutt, C.R., Howe, A.J.: Forward facing spike effects of bodies of different cross section in supersonic flow. Aeronaut. J. R. Aeronaut. Soc. 93(6), 229-234 (1989).
  • 7Milicevl SIS., Pavlovic, M.D., Ristic, S., Vitic, A.: On the influence of spike shape at supersonic flow past blunt bodies. Facta Univ. Ser. Mech. Autom. Control Robot. 3(12), 371-382 (2002).
  • 8Menezes, V., Saravanan, S., Jagadeesh, G., Reddy, K.RJ.: Experimental investigations of hypersonic flow over highly blunted cones with aerospikes. AIAA J. 41(10), 1955-1961 (2003).
  • 9Wang Ten-See,Chen Yen-Sen,Liu Ji-wen,et al.Advanced performance modeling of experimental laser lightcrafts[R].AIAA 2001-0648.
  • 10Molina-Morales P,Toyoda K,Komurasaki K,et al.CFD simulation of a 2-kW class laser thrust[R].AIAA 2001-0650.

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  • 1王福军.计算流体动力学分析[M].北京:清华大学出版社,2004.126-131,147-148.
  • 2M Y M Ahmed, N Qin. Recent advances in the aerothermodynamics of spiked hypersonic vehicles[J]. Progress in Aerospace Sciences, 2011, 47(6): 425-449.
  • 3A M Tahsini. Heat release effects on drag reduction in high speed flows[J]. Internat J Heat Mass Tran, 2013, 57(2): 657-661.
  • 4L N Myrabo, Y P Raizer. Laser-induced air spike for advanced transatmospheric vehicles[J]. AIAA 94-2451, 1994.
  • 5M A S Minucci, P G P Toro, A C Oliveira, et al: Flow visualization of laser induced air spikes in hypersonic flow[C]. AIP Conf Proc, 2005, 766: 514-527.
  • 6I I Salvador, M A S Minucci, P G Toro, et al: Experimental analysis of heat flux to a blunt body in hypersonic flow with upstream laser energy deposition-preliminary results[C]. AIP Conf Proc, 2006, 830: 163-171.
  • 7David Riggins, H F Nelson, Eric Johnson. Blunt-body wave drag reduction using focused energy deposition[J]. AIAA J, 1999, 37(4): 460-467.
  • 8T M Taylor, A Khamooshi, D W Riggins. Innovative concepts for large-scale drag and heat transfer reductions in high-speed flows [C]. Proceedings of t.he 44th AIAA Aerospace Sciences Meeting, 2006, 11: 7850-7871.
  • 9P Yu Georgievskii, V A Levin. Control of the flow past bodies using localized energy addition to the supersonic oncoming flow[J]. Fluid Dynamics, 2003, 38(5): 794-805.
  • 10V M Fomin, P K Tretyakov, J P Taran. Flow control using various plasma and aerodynamics approaches[J]. Aerosp Sci and Technol, 2004, 8(5): 411-421.

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