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Large-Eddy Simulation of Autoignition-Dominated Supersonic Combustion

机译:自燃为主的超音速燃烧的大涡模拟

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The simulation of low-speed combustion flows is well established. However, at highspeed conditions where radical formation and ignition delay are important, there is much less experience with turbulent combustion modeling. In the present work, a novel evolution variable manifold (EVM) approach of Cymbalist and Dimotakis is implemented in a production CFD code and preliminary RANS and large-eddy simulations are computed for a hydrogen combustion test case. The EVM approach solves a scalar conservation equation for the induction time to represent ignition delay. The state of the combustion products is tabulated as a function of density, energy, mixture fraction, and the evolution variable. A thermodynamically-consistent numerical flux function is developed and the approach for coupling the EVM table to CFD is discussed. Initial simulations show that the EVM approach produces good agreement with full chemical kinetics model simulations. Work remains to be done to improve the numerical stability, extend the grid, and increase the order of accuracy of the simulations.
机译:充分建立了低速燃烧流的模拟。但是,在需要自由基形成和点火延迟很重要的高速条件下,进行湍流燃烧建模的经验要少得多。在目前的工作中,在生产CFD代码中实施了Cymbalist和Dimotakis的新型演化可变流形(EVM)方法,并针对氢燃烧测试案例计算了初步的RANS和大涡模拟。 EVM方法解决了诱导时间的标量守恒方程,以表示点火延迟。燃烧产物的状态以密度,能量,混合比和演化变量的函数形式制成表格。建立了热力学上一致的数值通量函数,并讨论了将EVM表耦合到CFD的方法。初始仿真表明,EVM方法与完整的化学动力学模型仿真具有很好的一致性。仍有工作要做,以提高数值稳定性,扩展网格并增加仿真精度的顺序。

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