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HYPERSONIC RAREFIED FLOWS DSMC ANALYSIS BY A SIMPLIFIED CHEMICAL MODEL

机译:用简化的化学模型对超音速流动进行DSMC分析

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A simplified model for the analysis of molecular and reaction dynamics in hypersonic flows of rarefied gases is used to investigate the influence of oxygen dissociation in the prediction of aerothermal coefficients. The model is a direct simulation Monte Carlo method derived from the Larsen-Borgnakke method for the analysis of inelastic collisions. Tests performed in conditions near to re-entry conditions at an altitude of 115 km show significant effects of chemical reactions on the evaluation of the heat-transfer coefficient, while no real influence is found on lift and drag coefficients. Good agreement is found with results achieved using more sophisticated chemical models, as a 4 % maximum difference arises in the determination of surface quantities in re-entry conditions at 160 km. [References: 12]
机译:一种简化的模型,用于分析稀薄气体高超声速流动中的分子和反应动力学,以研究氧离解对预测空气热系数的影响。该模型是从拉尔森-博格纳克法(Larsen-Borgnakke method)导出的直接模拟蒙特卡洛方法,用于分析非弹性碰撞。在115 km高度接近再入条件的条件下进行的测试表明,化学反应对传热系数的评估有显着影响,而对升力和阻力系数没有真正的影响。在使用更复杂的化学模型获得的结果中发现了很好的一致性,因为在160 km的重入条件下确定表面量时最大差异为4%。 [参考:12]

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