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打算跨音速计算M6机翼，之前一直用的是不可压求解器，对可压求解器不是很熟悉。尝试用可压求解器算一个二维翼型的跨音速状态，但收敛性不太好。fluent中有基于密度的求解器，计算效果不错，Openfoam有类似的吗？
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