欧拉流体中边界层的发展,其 "激活 "反应类似于纳维-斯托克斯流体

P. A. Gazca-Orozco, J. Málek, K. R. Rajagopal
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引用次数: 0

摘要

我们考虑了一种流体的流动问题,这种流体的响应特性因速度梯度对称部分的规范值而改变,在临界值以下表现为欧拉流体,在临界值及以上表现为纳维-斯托克斯流体,规范值由外部刺激决定。我们的研究表明,这种流体在流过崖体时会形成边界层,这些边界层实际上与普朗特提出的经典边界层理论所遇到的边界层相同。经典边界层理论是在纳维-斯托克斯理论的背景下产生的近似值,与之不同的是,这里边界层的形成是由于构成关系的响应特性发生了变化。我们研究了这种流体流过机翼的情况,并与纳维-斯托克斯方程的解法进行了比较。我们发现,两种情况下的速度场和涡度场结果非常一致。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Development of boundary layers in Euler fluids that on “activation” respond like Navier–Stokes fluids

We consider the flow of a fluid whose response characteristics change due the value of the norm of the symmetric part of the velocity gradient, behaving as an Euler fluid below a critical value and as a Navier–Stokes fluid at and above the critical value, the norm being determined by the external stimuli. We show that such a fluid, while flowing past a bluff body, develops boundary layers which are practically identical to those that one encounters within the context of the classical boundary layer theory propounded by Prandtl. Unlike the classical boundary layer theory that arises as an approximation within the context of the Navier–Stokes theory, here the development of boundary layers is due to a change in the response characteristics of the constitutive relation. We study the flow of such a fluid past an airfoil and compare the same against the solution of the Navier–Stokes equations. We find that the results are in excellent agreement with regard to the velocity and vorticity fields for the two cases.

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