This paper documents the CFL3D contribution to the AIAA Supersonic Shock Boundary Layer Interaction Workshop, held in Orlando, Florida in January 2010. CFL3D is a Reynolds-averaged Navier-Stokes code. Four shock boundary layer interaction cases are computed using a one-equation turbulence model widely used for other aerodynamic problems of interest. Two of the cases have experimental data available at the workshop, and two of the cases do not. The effect of grid, flux scheme, and thin-layer approximation are investigated. Comparisons are made to the available experimental data. All four cases exhibit strong three-dimensional behavior in and near the interaction regions, resulting from influences of the tunnel side-walls.
CFL3D Contribution to the AIAA Supersonic Shock Boundary Layer Interaction Workshop
2010-10-01
Report
Keine Angabe
Englisch
NTRS
|Overview of the 2010 AIAA Shock Boundary Layer Interaction Prediction Workshop
British Library Conference Proceedings | 2010
|LES for Separated Supersonic Turbulent Boundary Layer and Shock Interaction (AIAA 2014-0437)
British Library Conference Proceedings | 2014
|