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Piloted ignition of solid fuels in turbulent back-step flows

机译:湍流逆流中的固体燃料先导点火

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Piloted ignition of solid fuels in dump combustor geometry subject to an igniter hot jet plume is numerically investigated. The objective of this work is to gain insight into the fuel ignition and subsequent flame spreading in this turbulent flow configuration. Conjugate heat transfer between gas and solid phases is considered to study the solid fuel heating and evaporation process; Solid phase energy equation is simultaneously solved coupled with flow governing equations. Finite rate one step second order chemistry is used in simulations. The gas phase equations along with the Spalart-Allmaras turbulence model are solved with a finite volume approach in which the AUSM~+ scheme is used to calculate the convective fluxes. The overall ignition delay time and flame spreading rate are predicted under a typical igniter operation. The results show that choosing a stronger igniter for reducing the ignition delay time does not necessarily guaranty the perfect firing process.
机译:数值研究了在引燃器热射流羽流作用下的排污燃烧室几何形状中的固体燃料先导点火。这项工作的目的是深入了解这种湍流配置中的燃料着火和随后的火焰蔓延。考虑了固相之间的共轭传热,以研究固体燃料的加热和蒸发过程。固相能量方程与流量控制方程同时求解。在模拟中使用有限速率的一阶二阶化学。气相方程和Spalart-Allmaras湍流模型一起使用有限体积方法求解,其中使用AUSM〜+方案计算对流通量。在典型的点火器操作下,可以预测总的点火延迟时间和火焰蔓延速率。结果表明,选择更强的点火器以减少点火延迟时间并不一定能保证完美的点火过程。

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