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高超声速气动试验的新进展 被引量:5

THE NEW PROGRESS OF HYPERSONIC AERODYNAMIC AND AEROTHERMODYNAMIC TESTING
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摘要 本文报导了1992年7月在美国纳希维尔召开的 AIAA 第17届航空航天地面试验会议的概况。简要地介绍了讨论航空航天地面试验面临的技术挑战,CFD 和地面试验的相互作用,美国气动力学与气动热力学研究的未来等三个大会报告的内容。介绍了在会议报告中叙述的对高超声速气动试验的新要求和自由飞弹道靶、 脉冲风洞、稀薄气体设备、电弧加热器的新进展。最后,对我国高超声速气动试验的发展提出了建议。 The survey of 17th AIAA Aerospace Ground Testing Con-ference to have been held in Nashvill USA,July 1992 is reported in thispaper.The situation of three plenary session that discussed the technicalchallenges facing aerospace ground-based testing,interaction of CFD andground-based testing and future of aerodynamic/aerothermodynamic re-search in USA,is introduced briefly.The future requirements for hypersonic aerodynamic and aerother-modynamictesting and the new progress of ballistic ranges,impulse windtunnels,rarefied flow facilities and arc heaters to have been describedin the papers of this conference are presented.The suggestions for thedevelopment of hypersonic aerodynamic and aerothermodynamic testingin our country are put forward.
作者 黄志澄
出处 《气动实验与测量控制》 CSCD 1993年第1期1-13,共13页
关键词 地面试验 高超声速 空气动力学 aerospace ground testing hypersonic aerodynamics aerothermodynamics ballistic range shock tunnel low density wind tunnel arc heater
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  • 1郑红梅,刘正士.机器人六维腕力传感器动态性能标定系统的研究[J].电子测量与仪器学报,2006,20(3):88-92. 被引量:11
  • 2张德丰.基于小波的信号突变点检测算法研究[J].计算机工程与科学,2007,29(12):98-100. 被引量:17
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  • 5Naumann K, Ende H, Mathieu G, et al. Millisecond aerodynamic force measurement with side-jet model in the ISL shock tunnel. AIAA Journal, 1993, 31 (6): 1068-1074.
  • 6Naumann K, Ende H. A novel technique for aero- dynamic force measurements in shock tubes. AlP Conference Proceedings, 1990, 208:653-658.
  • 7Joarder R, Jagadeesh G. A new free-floating accelerometer balance system for force measurements in shock tunnels. Shock Waves, 2003, 13:409-412.
  • 8Saravanan S, Jagadeesh G, Reddy KPJ. Aerodynamic force mea-surement using 3-component accelerometer force balance system in a hypersonic shock tunnel. Shock Waves, 2009, 18:425-435.
  • 9Niranjan S, Mahapatra DR, Jagadeesh G, et al. An acceleromet balance system for measurement of aerodynamic force coefficienl over blunt bodies in a hypersonic shock tunnel. Meas Sci Techno 2003, 14:260-272.
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