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目前在做航空发动机点火过程的数值模拟,前期一直采用ANSYS Fluent中LES+DPM+EDC模型进行仿真,点火源采用高温+高速的射流来简化,结果发现燃烧只能在射流头部发生,燃烧无法进一步扩展到整个燃烧室中,初步判断可能是燃烧模型的问题,但是目前Fluent只有EDC模型才能进行点火过程的仿真,所以想咨询各位前辈OF中是否有相对合适的Solver和燃烧模型来模拟喷雾点火过程。十分感谢!
这里有一个点火的模型可以使用:Github