Direct Numerical Simulation of the Turbulent Ekman Layer: Evaluation of Closure Models

Stuart Marlatt Department of Aerospace Engineering Sciences, University of Colorado, Boulder, Colorado

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Scott Waggy Department of Aerospace Engineering Sciences, University of Colorado, Boulder, Colorado

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Sedat Biringen Department of Aerospace Engineering Sciences, University of Colorado, Boulder, Colorado

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Abstract

A direct numerical simulation (DNS) at a Reynolds number of 1000 was performed for the neutral atmospheric boundary layer (ABL) using the Ekman layer approximation. The DNS results were used to evaluate several closure approximations that model the turbulent stresses in the Reynolds averaged momentum equations. Two first-order closure equations proposed by O’Brien and by Large, McWilliams, and Doney were tested; both models approximate the eddy diffusivity as a function of height using cubic polynomials. Of these two models, the O’Brien model, which requires data both at the surface layer and at the top of the boundary layer, proved superior. The higher-order kε model also agreed well with DNS results and more accurately represented the eddy diffusivity in this rotational flow.

Current affiliation: United Launch Alliance, Littleton, Colorado.

Corresponding author address: Sedat Biringen, Aerospace Engineering Sciences, CB 429, University of Colorado, Boulder, CO 80309. E-mail: biringen@colorado.edu

Abstract

A direct numerical simulation (DNS) at a Reynolds number of 1000 was performed for the neutral atmospheric boundary layer (ABL) using the Ekman layer approximation. The DNS results were used to evaluate several closure approximations that model the turbulent stresses in the Reynolds averaged momentum equations. Two first-order closure equations proposed by O’Brien and by Large, McWilliams, and Doney were tested; both models approximate the eddy diffusivity as a function of height using cubic polynomials. Of these two models, the O’Brien model, which requires data both at the surface layer and at the top of the boundary layer, proved superior. The higher-order kε model also agreed well with DNS results and more accurately represented the eddy diffusivity in this rotational flow.

Current affiliation: United Launch Alliance, Littleton, Colorado.

Corresponding author address: Sedat Biringen, Aerospace Engineering Sciences, CB 429, University of Colorado, Boulder, CO 80309. E-mail: biringen@colorado.edu
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