Parallel URANS Simulations of an Axisymmetric Jet in Cross-Flow
R.K. Agarwalrka@mc.wustl.edu; J. Cui, * Department of Mechanical and Aerospace Engineering, Washington University, One Brookings Drive, St. Louis, MO 63130-4899
Abstract
An Unsteady Reynolds-Averaged Navier-Stokes (URANS) solver - WIND is employed to compute the flow field of an axisymmetric synthetic jet in cross-flow. This flow field corresponds to case 2 of NASA Langley Research Center Workshop "CFD validation of synthetic jets and turbulent separation control" held at Williamsburg, VA in March 2004. Parallel Three-dimensional simulations have been performed by employing the appropriate boundary conditions at the diaphragm of the actuator using Shear-Stress Transport (SST), Spalart-Allamaras ...
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