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Utilizing unsteady curved detonation analysis and detailed kinetics to study the direct initiation of detonation in H_2-O_2 and H_2-Air mixtures

机译:利用非定常弯曲爆轰分析和详细的动力学研究H_2-O_2和H_2-空气混合物中的直接起爆

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In the present paper, utilizing a detailed chemical kinetics, the simplified unsteady reactive Euler equations are solved in the reaction zone of a curved detonation, to derive the relation between detonation propagation velocity (D) with its acceleration (D) and front curvature (k), that is the so called D - D - k relation. Then, this relation is used for tracking the detonation front and to study the onset of a self sustained near CJ detonation. The reaction-zone history is studied to understand the events that happen during the onset of a detonation in Hydrogen/Oxygen mixtures. It is observed that the relative movement of the location of the peak of the thermicity function with respect to the front, and its absolute value, are two parameters that determine the physics of the onset.rnUtilizing the D - D - k relation based on the detailed chemical kinetics, the critical initiation energy is calculated for the H_2-O_2 and H_2-Air mixtures. Although, the previous studies by single step kinetics [A. R. Kasimov, PhD Thesis, Univ. of Illinois at Urbana-Champaign] and the present results both predict the critical initiation energy with acceptable accuracy, however, the present work makes a better prediction of the equivalence ratio at which the H_2-O_2 mixture experiences its minimum critical energy. Also the present predictions are more accurate for the lean H_2-O_2 and H_2-Air mixtures. Using the present method, the effect of initial pressure on the critical initiation energy of H_2-O_2 mixture is well predicted compared to empirical results.
机译:在本文中,利用详细的化学动力学,在弯曲爆轰的反应区域中求解了简化的非稳态反应欧拉方程,从而得出了爆轰传播速度(D)与加速度(D)和前曲率(k)之间的关系。 ),即所谓的D-D-k关系。然后,该关系用于跟踪爆轰前沿并研究自持续近CJ爆轰的发生。研究反应区的历史以了解氢气/氧气混合物中爆炸开始时发生的事件。可以观察到,热学函数峰的位置相对于前沿的相对运动及其绝对值是确定发作物理性质的两个参数。详细的化学动力学,计算了H_2-O_2和H_2-空气混合物的临界引发能。虽然,以前的研究是通过单步动力学[A. R. Kasimov,大学博士学位论文。和目前的结果均以可接受的精度预测了临界起始能,但是,本工作更好地预测了H_2-O_2混合物经历其最低临界能的当量比。此外,对于稀薄的H_2-O_2和H_2-空气混合物,当前的预测更为准确。使用本方法,与经验结果相比,可以很好地预测初始压力对H_2-O_2混合物的临界起始能的影响。

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