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Experiments in a Combustion-Driven Shock Tube with an Area Change

机译:在燃烧驱动的冲击管中进行面积变化的实验

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This data demonstrates the shock tube's potential for use as a part of a small hypersonic test facility and to test fundamental gas physics. Bakos uses a figure of merit of a total enthalpy of 15.2 MJ/kg for the driver section of an expansion tunnel to produce physically relevant flows. Reservoir enthalpies in excess of 18 MJ/kg can be regularly produced in this shock tube. The Cantera simulation of the shock tube also reveals that the gas behind both incident and reflected shocks is highly dissociated, even at the lower shock Mach numbers in the operational range of the facility. This affords an opportunity for inexpensive investigations of gas dynamics.
机译:该数据证明了冲击管在小型高超音速测试设备中的用途以及测试基本气体物理的潜力。 Bakos使用总焓为15.2 MJ / kg的品质因数来计算膨胀隧道的驱动器部分,以产生与物理相关的流量。在该激波管中,经常会产生超过18 MJ / kg的储层焓。激振管的Cantera模拟结果还表明,即使在工厂运行范围内的激振马赫数较低的情况下,入射激波和反射激波背后的气体也会高度分解。这为廉价的气体动力学研究提供了机会。

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