首页> 外文会议>AIAA 32nd Aerospace Sciences Meeting Exhibit January 10-13, 1994/Reno, NV >An experimental and computational study of unsteady supersonic 2-D open cavity flow physics
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An experimental and computational study of unsteady supersonic 2-D open cavity flow physics

机译:非定常超声速二维开腔流场的实验与计算研究

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This paper is an experimental/computational analysis of the transient fluid dynamic mechanisms inherent in open cavity flow fields. The goal of the current research is to develop a physically verifiable description of the two-dimensional transient shear layer oscillation cycle mechanisms associated with open cavity flow fields. This has been accomplished by conducting experiments over a large width to length ratio cavity to simulate two-dimensional flow and by performing two-dimensional numerical simulations. A two dimensional open cavity oscillation cycle is described.
机译:本文是对开腔流动场固有的瞬态流体动力机制的实验/计算分析。目前研究的目标是开发与开腔流动场相关联的二维瞬态剪切层振荡循环机构的物理可靠描述。这是通过在大宽度的实验到长度比腔中进行实验来实现,以模拟二维流动并通过执行二维数值模拟。描述了两个尺寸的开腔振荡循环。

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