44th AIAA Aerospace Sciences Meeting and Exhibit · 2006 · 94 citations · 67 references
EngineeringAerospace EngineeringComputational EngineeringAerodynamicsComputational Fluid DynamicsFluid DynamicsComputational AerodynamicsDirect Numerical SimulationLarge-eddy SimulationShock WavesTurbulenceTurbulent FlowBoundary-layer SeparationNumerical ModelingNumerical SimulationReynolds-averaged Navier-stokes EquationsShock - Boundary-layer InteractionShock Wave-boundary Layer InteractionShock-boundary Layer InteractionShock-boundary-layer Interaction
A critical analysis of some recent experimental and computational research of 2-D and 3-D shock wave/turbulent boundary layer interaction (SWTBLI) is carried out. The specific stages of turbulent boundary layer separation development in a vicinity of compression ramps, forward- and backward- facing steps, one- and double-fin configurations are considered. The flowfield topology and principal physical processes are analyzed and specified for different cases of SWTBLI. The examples of modern numerical modeling on a basis of the Reynolds-averaged Navier-Stokes equations with various turbulence models as well as Direct Numerical Simulation (DNS) and Large Eddy Simulation (LES) are demonstrated and compared. The perspectives and problems of future SWTBLI studies are discussed.
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Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next?
David Dolling · AIAA Journal · 2001 · 1.1K citations
On the k-3 stagnation point anomaly
Paul A. Durbin · International Journal of Heat and Fluid Flow · 1996 · 508 citations · Full text