A Model of a Turbulent Boundary Layer With a Non-Zero Pressure Gradient
G. I. Barenblatt, A. J. Chorin, and V. M. Prostokishin

TL;DR
This paper presents a model of turbulent boundary layers with pressure gradients, identifying two distinct self-similar regions and how their scaling laws depend on pressure gradient and Reynolds number, supported by experimental data.
Contribution
The authors introduce a two-region model for turbulent boundary layers with pressure gradients, detailing how scaling laws vary with pressure conditions and Reynolds number, supported by experimental validation.
Findings
The power law exponent $eta$ varies with pressure gradient sign.
Adverse pressure gradients increase $eta$, favorable decrease it.
Experimental data aligns with the proposed model.
Abstract
According to a model of the turbulent boundary layer proposed by the authors, in the absence of external turbulence the intermediate region between the viscous sublayer and the external flow consists of two sharply separated self-similar structures. The velocity distribution in these structures is described by two different scaling laws. The mean velocity u in the region adjacent to the viscous sublayer is described by the previously obtained Reynolds-number-dependent scaling law , , , . (Here is the dynamic or friction velocity, y is the distance from the wall, the kinematic viscosity of the fluid, and the Reynolds number is well defined by the data) In the region adjacent to the external flow the scaling law is different:…
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Taxonomy
TopicsFluid Dynamics and Turbulent Flows · Computational Fluid Dynamics and Aerodynamics · Navier-Stokes equation solutions
