Toward low‐noise synthetic turbulent inflow conditions for aeroacoustic calculations |
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Authors: | Adrian Sescu Ray Hixon |
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Affiliation: | 1. Department of Aerospace Engineering, Mississippi State University, , MS 39762, USA;2. MIME Department, University of Toledo, , MS 312, Toledo, OH 43606, USA |
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Abstract: | The accuracy of boundary conditions for computational aeroacoustics is a well‐known challenge, due in part to the necessity of truncating the flow domain and replacing the analytical boundary conditions at infinity with numerical boundary conditions. In particular, the inflow boundary condition involving turbulent velocity or scalar fields is likely to introduce spurious waves into the domain, therefore degrading the flow behavior and deteriorating the physical acoustic waves. In this work, a method to generate low‐noise, divergence‐free, synthetic turbulence for inflow boundary conditions is proposed. It relies on the classical view of turbulence as a superposition of random eddies convected with the mean flow. Within the proposed model, the vector potential and the requirement that the individual eddies must satisfy the linearized momentum equations about the mean flow are used. The model is tested using isolated eddies convected through the inflow boundary and an experimental benchmark data for spatially decaying isotropic turbulence. Copyright © 2013 John Wiley & Sons, Ltd. |
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Keywords: | turbulent flow synthetic turbulence aeroacoustics large eddy simulations (LES) inflow boundary conditions, finite difference |
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