Three-dimensional(3D)unsteady compressible flow over an open cavity and the relevant aeroacoustics are studied using a hybrid LES-acoustic analogy method.
使用大涡模拟-声学比拟相结合方法,研究三维开式空腔非定常可过及其相关气声学问题。
Three-dimensional(3D)unsteady compressible flow over an open cavity and the relevant aeroacoustics are studied using a hybrid LES-acoustic analogy method.
使用大涡模拟-声学比拟相结合方法,研究三维开式空腔非定常可过及其相关气声学问题。
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