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An experimental and computational study of the mechanisms of detonation transmission in layered hydrogen-oxygen mixtures.

机译:层状氢氧混合物中爆轰传递机理的实验和计算研究。

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This thesis presents the results of an experimental, analytical, and numerical investigation of the mechanisms of {dollar}rm Hsb2{dollar}-{dollar}rm Osb2{dollar} detonation transmission. The experimental configuration is designed to study how a detonation originally propagating into one gaseous mixture of hydrogen and oxygen (primary) is transmitted laterally into a secondary mixture. The configuration and the mixtures used for the experimental and numerical investigations are similar so that the experimental and the numerical results can be compared directly.; The experiments are conducted using mixtures with varying equivalence ratios. A stable wave configuration consisting of an oblique shock and an oblique detonation is observed, and three modes of ignition are identified and explained. The analytical results are based on a shock-polar analysis of the steady-state model for the waves in the primary and secondary mixtures, using the two-gamma method of Liou (1986) to derive the jump conditions across the shocks and detonation waves. The analytical method helps interpreting and predicting the experimental results, provided that steady state is achieved. However, numerical simulations are required for the analysis of the early, unsteady part of the transmission.; An improved chemical model for {dollar}rm Hsb2{dollar}-{dollar}rm Osb2{dollar} combustion is developed and used in one and two-dimensional numerical simulations of detonation waves. The one-dimensional calculations are used to simulate the propagation of a planar detonation wave in a shock tube. The tests of the numerical and physical parameters show that the numerical results agree to within a few percent with the theory of one-dimensional CJ detonations. Two-dimensional simulations of the detonation transmission experiments using the improved chemical model are conducted for the case where both the primary and the secondary mixtures are stoichiometric. In the calculations, the secondary mixture does not ignite behind the transmitted blast wave and the primary detonation gets quenched. Both the absence of ignition in the secondary mixture and the quenching of the primary detonation result from the long ignition times characteristic of the background fluid.; In the experiments conducted with both primary and secondary mixtures stoichiometric, the secondary mixture always ignited directly behind the transmitted blast wave. There are at least three possible explanations for the lack of agreement between the numerical and the experimental results: the kinetic model, the physical model (e.g., the transverse waves were not resolved), and discrepancies between the experimental and the simulated problems (e.g., possible presence of three-dimensional effects). These factors suggest that the agreement between the numerical and the experimental results should be improved by increasing the accuracy of the high-pressure kinetic model and the numerical resolution.
机译:本文介绍了对{rm} rm Hsb2 {dollar}-{dollar} rm Osb2 {dollar}爆轰传递机理进行实验,分析和数值研究的结果。实验配置旨在研究最初传播为氢和氧的一种气态混合物(一次)的爆炸如何横向传输到二次混合物中。实验和数值研究所用的构型和混合物相似,因此可以直接比较实验和数值结果。使用具有不同当量比的混合物进行实验。观察到了由倾斜冲击和倾斜爆震组成的稳定波形,并确定并说明了三种点火方式。分析结果是基于对主要混合物和次要混合物中波的稳态模型的冲击极点分析,并使用Liou(1986)的双伽马方法得出了冲击波和爆震波的跳跃条件。只要达到稳定状态,该分析方法有助于解释和预测实验结果。但是,需要数值模拟来分析变速箱的早期,不稳定部分。建立了一种改进的化学模型,用于燃烧波的燃烧,并在一维和二维数值模拟中将其用于爆轰波。一维计算用于模拟平面爆震波在激波管中的传播。数值和物理参数测试表明,数值结果与一维CJ爆轰理论相吻合。对于主要混合物和次要混合物都是化学计量的情况,使用改进的化学模型进行了爆轰传递实验的二维模拟。在计算中,次要混合物不会在发射的爆炸波后面点燃,一次起爆被淬灭。次级混合物中没有点火和初级爆炸的猝灭都是由于背景流体的长点火时间特性造成的。在用化学计量的主要和次要混合物进行的实验中,次要混合物总是直接在爆炸冲击波后面点燃。对于数值结果与实验结果之间的不一致,至少存在三种可能的解释:动力学模型,物理模型(例如,横波未解决)以及实验问题与模拟问题之间的差异(例如,可能存在三维效果)。这些因素表明,应通过增加高压动力学模型的精度和数值分辨率来改善数值结果与实验结果之间的一致性。

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