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Quasi One Dimensional Modeling of Rotational Detonation Engines

机译:旋转爆震发动机的准一维建模

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Rotating detonation engines have received renewed interest in recent years and a number of groups around the world are pursuing developments for a variety of aerospace missions. The dynamic behavior of the injection system imposed by passage of one or multiple waves in the combustion chamber leads to complex combustion wave dynamics that are still defying understanding. Wave topology changes, slapping modes, and even alterations in wave direction have been observed experimentally. The objective of this study is to assemble a simple analysis tool for investigation of these phenomena and to ultimately inform on overall engine operabilty characteristics. The model employs a 1-D solution of the azimuthal wave dynamics with a global reaction mechanism coupled to lumped paramenter domains that dynamically feed the detonation region with reactants of varying stoichiometry. Model elements are described and some initial solutions are provided to demonstrate the characteristics of the newly-developed tool.
机译:近年来,旋转爆震发动机引起了人们的新兴趣,世界各地的许多团体正在为各种航空航天任务寻求发展。由一个或多个波在燃烧室中通过而施加的喷射系统的动态行为导致仍然难以理解的复杂的燃烧波动力学。实验观察到波的拓扑结构变化,拍击模式甚至波向发生变化。这项研究的目的是组装一个简单的分析工具,以研究这些现象,并最终告知整体发动机的运行特性。该模型采用了方位角动力学的一维解决方案,其中的全局反应机制耦合到集总的Paramenter域,该域动态地向爆炸区域提供化学计量不同的反应物。描述了模型元素,并提供了一些初始解决方案来演示新开发工具的特性。

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