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谢谢版主！我换成瞬态试一试！
风力机翼型，使用Fluent在Re=107，SST K-w模型进行计算，最多只能计算从-5~22°的气动参数，更大的攻角就很难再收敛，残差出现周期性波动，是因为湍流更加复杂了吗？想请教一下各位老师，有什么办法能在更大的攻角范围（±30°）得到气动参数呢？
