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Asymptotic Model of the Development of Separations inside a Boundary Layer under the Action of a Traveling Pressure Wave

机译:行进压力波作用下边界层内分离发展的渐近模型

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摘要

A model of the nonlinear interaction between a pressure perturbation traveling at a constant velocity and an incompressible boundary layer is constructed when its near-wall part is described by the "inviscid boundary layer" equations. A steady-state solution is managed to obtain in the finite form under the assumption that it exists in a moving coordinate system. It is shown that the boundary layer can easily overcome pressure perturbations whose amplitude is not higher than the dynamic pressure calculated from the velocity of the pressure perturbation. At the higher pressure perturbation amplitudes a vortex sheet sheds from the body surface to the boundary layer. The vortex sheet represents an unstable surface of the tangential discontinuity which separates the regions of the direct and reverse separation flows. In the case of an arbitrary shape of the pressure perturbation the surface of the tangential discontinuity sheds from the body surface at a finite angle with the formation of a stagnation point. An example of the pressure perturbation in which the vortex sheet sheds from the body surface along the tangent is constructed.
机译:当用“无粘性边界层”方程描述其近壁部分时,建立了以恒定速度传播的压力扰动和不可压缩边界层之间的非线性相互作用模型。假设在运动坐标系中存在稳态解,则以有限形式进行管理。结果表明,边界层可以容易地克服振幅不大于由压力扰动速度计算出的动态压力的压力扰动。在较高的压力扰动振幅下,涡旋片从体表表面流到边界层。涡旋片表示切向不连续的不稳定表面,该表面将正向和反向分离流的区域分开。在压力扰动为任意形状的情况下,切向不连续面会以有限的角度从体表脱落,并形成停滞点。构造了一个压力扰动的例子,其中涡旋片沿着切线从身体表面脱落。

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