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首页> 外文会议>International Symposium on Beamed Energy Propulsion >Development of a New Hypersonic Shock Tunnel Facility to Investigate Electromagnetic Energy Addition for Flow Control and Basic Supersonic Combustion
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Development of a New Hypersonic Shock Tunnel Facility to Investigate Electromagnetic Energy Addition for Flow Control and Basic Supersonic Combustion

机译：开发新的超音速冲击隧道设施，以研究流量控制和基本超声燃烧的电磁能量添加

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A new 0.6-m. diameter Hypersonic Shock Tunnel is been designed, fabricated and will be installed at the Laboratory of Aerothermodynamics and Hypersonics IEAv-CTA, Brazil. The brand new hypersonic facility, designated as T3, is primarily intended to be used as an important tool in the investigation of supersonic combustion management and of electromagnetic energy addition for flow control. The design of the runnel enables relatively long test times, 2–10 milliseconds, suitable for basic supersonic combustion and energy addition by laser experiments. Free stream Mach numbers ranging from 6 to 25 can be produced and stagnation pressures and temperatures of 200 atm. and 5,500 K, respectively, can be generated. Shadowgraph and schlieren optical techniques will be used for flow visualization and the new facility is expected to be commissioned by the end of 2006.
机译：新的0.6米。设计，制造，并将安装直径超声波震荡隧道，并将安装在空中动力学和高疗效IEAV-CTA，巴西的实验室。作为T3指定的全新超音速设施主要用于调查超音速燃烧管理和用于流量控制的电磁能量的重要工具。脉冲的设计使得测试时间相对长，2-10毫秒，适用于激光实验的基本超音速燃烧和能量添加。可以产生6至25的自由流Mach编号，可以生产和停滞压力和200atm的温度。分别可以生成5,500 k。 ShadowGraph和Schlieren光学技术将用于流量可视化，预计新设施将在2006年底委托。

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