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타이틀	CFL3D Contribution to the AIAA Supersonic Shock Boundary Layer Interaction Workshop
저자	Rumsey, Christopher L.
Keyword	COMPUTATIONAL FLUID DYNAMICS;; MATHEMATICAL MODELS;; NAVIER-STOKES EQUATION;; SHOCK LAYERS;; SUPERSONIC BOUNDARY LAYERS;; TURBULENCE MODELS;; WALLS
URL	http://hdl.handle.net/2060/20100037235
보고서번호	NASA/TM-2010-216858
발행년도	2010
출처	NTRS (NASA Technical Report Server)
ABSTRACT	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.