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Pyrolysis in Porous Media: Numerical Analysis and Comparison to Experiments.

机译:多孔介质中的热解:数值分析和实验比较。

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Only limited studies are available experimentally to investigate hydrocarbon fuel pyrolysis, which can be of practical interest for the active cooling of head loaded components in aerospace vehicles such as combustors in rocket engines. The numerical simulation is an additional way to investigate the related phenomena (heat and mass transfer with chemistry). After a first code validation with experiments based upon inert gases, the code is further extended towards permeation with reactive dodecane and a reasonable agreement is found. The experimental accuracy of the permeability's' determination is confirmed numerically to be within ± 30 %. Numerically it is shown that this accuracy is due to strong flow spatial heterogeneities. The border effect of the test cell is found to be related to the permeable medium thickness whereas the temperature field is correlated to the reaction zone. Two different kinetic mechanisms are used to investigate the chemistry effect on the heat and mass transfer. They provide also a better analysis of the fuel pyrolysis and of the products' formation.
机译:只有有限的研究可以通过实验进行研究,以研究烃燃料热解,这对于在航空航天车辆中的头部装载部件的主动冷却可能具有实际兴趣,例如火箭发动机中的燃烧器。数值模拟是研究相关现象的额外方法(热量和化学传递)。在基于惰性气体的实验与实验的第一代码验证之后,该代码进一步延长了与反应十二烷的渗透,并找到合理的协议。渗透率的确定的实验准确性在数值上确认为±30%。在数值上表明,这种精度是由于强流量的空间异质性。发现测试电池的边界效应与渗透介质厚度有关,而温度场与反应区相关。两种不同的动力学机制用于研究对热量和传质的化学作用。它们还提供更好地分析燃料热解和产品的形成。

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