首页 | 本学科首页   官方微博 | 高级检索  
     


Toward low‐noise synthetic turbulent inflow conditions for aeroacoustic calculations
Authors:Adrian Sescu  Ray Hixon
Affiliation:1. Department of Aerospace Engineering, Mississippi State University, , MS 39762, USA;2. MIME Department, University of Toledo, , MS 312, Toledo, OH 43606, USA
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.
Keywords:turbulent flow  synthetic turbulence  aeroacoustics  large eddy simulations (LES)  inflow boundary conditions, finite difference
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号