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Analytical and experimental study of supersonic combustion of hydrogen in a vitiated airstream

机译:通风气流中氢超音速燃烧的分析和实验研究

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摘要

Detailed probe measurements of total temperature, pressure, and composition were taken in a two-dimensional test section 35.6 cm downstream of hydrogen injection. A high pressure gas generator supplied Mach 2.44 vitiated air or inert gas at elevated temperatures and at a static pressure equal to that of the hydrogen. Special water-cooled probes and sampling techniques were developed for the short test times required by heat-sink hardware. Independent methods of measuring stream total temperatures are compared. For the pure mixing case, the computed composition profile agreed well with the experimental profile. The analysis takes into account the wall boundary layer and the initial boundary layer in the main stream. Ignition of hydrogen, as determined from photographic exposures of the radiating gases, varied from 30 to 10 cm downstream from injection for a 45 K increase in local free-stream static temperature.
机译:在氢气注入下游35.6 cm的二维测试区域中,对总温度,压力和组成进行了详细的探针测量。高压气体发生器在升高的温度下和等于氢气的静压下提供2.44马赫的真空空气或惰性气体。开发了特殊的水冷探头和采样技术,以缩短散热器硬件所需的测试时间。比较了测量物流总温度的独立方法。对于纯混合情况,计算出的组成轮廓与实验轮廓吻合良好。该分析考虑了主流中的墙边界层和初始边界层。根据辐射气体的摄影曝光确定,氢气的点火在注入下游从30厘米到10厘米不等,局部自由流静态温度增加了45K。

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