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Development and application of reduced reaction mechanisms for modeling high-speed reacting flows.

机译:用于高速反应流建模的简化反应机制的开发和应用。

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Advanced high-speed vehicles require propulsive devices which minimize losses associated with slowing of the air stream before combustion. To achieve this goal, a better understanding of the mixing and combustion of high-speed reacting flow fields is essential. CFD analysis provides a valuable tool to accomplish this task, in particular predicting the ignition and flame-holding characteristics of supersonic reacting flows. Because of the large number of reactive species involved and because of the large Reynolds and Damkohler numbers associated with these flows, the computational requirements in modeling such flows are enormous. Based on flow and chemical time scales, systematically developed reduced reaction mechanisms that retain the finite-rate effects of a detailed chemical kinetic mechanism are used here as a method of simplifying this effort, without loss of accuracy. For an oblique detonation wave, established by a supersonic flow of stoichiometric mixture of hydrogen and air past a wedge, three reduced-reaction mechanisms are developed by introducing steady-state approximations for the species OH, O and HO{dollar}sb2,{dollar} and implemented in a computer code that uses a MacCormack like scheme to integrate the governing equations. The induction length in the oblique detonation wave, along with the temperature and species profiles, predicted with the detailed and the reduced reaction mechanisms are used to measure the accuracy of the reduced reaction models developed. These models are also implemented in a static reactor model to test the ignition delay predictions under various conditions. Comparisons indicate a good agreement between the detailed solution and the reduced reaction mechanism solutions, indicating the validity of the approximations introduced. The static reactor model is also used to develop a reduced reaction mechanism for modeling the ignition phenomena of a mixture containing a "representative endothermic fuel" and air, to demonstrate the versatility of this approach. For this mixture, the ignition delay predictions obtained with the reduced reaction model are in excellent agreement with the predictions obtained with the detailed model.
机译:先进的高速车辆需要推进装置,以使与燃烧前空气流减慢相关的损失最小化。为了实现这一目标,必须更好地理解高速反应流场的混合和燃烧。 CFD分析提供了完成此任务的宝贵工具,尤其是预测超音速反应流的着火和火焰保持特性。由于涉及大量的反应物种,并且由于与这些流相关的雷诺数和达姆科勒数较大,因此对此类流进行建模的计算需求量很大。基于流量和化学时间尺度,在这里使用保留详细化学动力学机制的有限速率效应的系统开发的减少的反应机制,作为简化此工作而不损失准确性的方法。对于由氢和空气经过楔形物的化学计量混合物的超音速流建立的倾斜爆轰波,通过引入OH,O和HO的稳态近似值,开发了三种还原反应机理。 }并在使用类似于MacCormack的方案的计算机代码中集成控制方程。倾斜爆轰波的感应长度,以及温度和物种分布,通过详细的和简化的反应机理进行预测,可用来测量所开发的还原反应模型的准确性。这些模型还可以在静态反应堆模型中实施,以测试各种条件下的点火延迟预测。比较表明详细解法和简化的反应机理解之间有很好的一致性,表明引入的近似方法的有效性。静态反应器模型还用于开发简化的反应机理,以对包含“代表性吸热燃料”和空气的混合物的着火现象进行建模,以证明该方法的多功能性。对于这种混合物,使用简化的反应模型获得的点火延迟预测与通过详细模型获得的预测非常吻合。

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