Heat Transfer to Catalytic Surface in a Subsonic Jet of Nitrogen Plasma

A. Bryzgalov
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Abstract

Validation studies on the heat fluxes on water-cooled catalytic surfaces in subsonic flows of high-temperature dissociated nitrogen are presented. Simulations are performed for the conditions of experiments performed in the IGP-4 plasmatron available in IPMech RAS for four operating powers and three test materials with known catalytic recombination coefficients. The computational model describes two-dimensional flow of chemically non-equilibrium nitrogen plasma. Stefan − Maxwell equations are applied to model multicomponent diffusion in the flow and on the catalytic surface. Reasonable agreement between the calculated and measured heat fluxes is demonstrated. It is shown that deviation of the results of the computational model from the ex-perimentally determined heat fluxes is generally within 15 % (the highest deviation is 29 %). Possible reasons for the deviation are discussed, and the dependence of heat fluxes on the kinetic scheme is demonstrated.
氮等离子体亚音速射流中催化表面的热传递
对高温解离氮亚音速流动中水冷催化表面的热流进行了验证研究。模拟了IPMech RAS中可用的IGP-4等离子体在四种工作功率和三种已知催化重组系数的测试材料下进行的实验条件。该计算模型描述了化学非平衡态氮等离子体的二维流动。Stefan−Maxwell方程用于模拟流动和催化表面上的多组分扩散。计算结果与实测结果吻合较好。计算结果表明,模型计算结果与实验测定的热通量偏差一般在15%以内(最高偏差为29%)。讨论了产生偏差的可能原因,并证明了热通量对动力学格式的依赖性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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