Publication | Closed Access
Large-Eddy Simulations of Idealized Shock/Boundary-Layer Interactions with Crossflow
20
Citations
39
References
2022
Year
AeroacousticsPrecursor BubbleUnsteady FlowEngineeringAerospace EngineeringFluid MechanicsTurbulence ModelingNumerical SimulationAerodynamicsBoundary-layer ThicknessThin Precursor SeparationComputational MechanicsMultiphase FlowIdealized Shock/boundary-layer InteractionsLarge Eddy SimulationBoundary LayerHydrodynamic Stability
An idealized shock/boundary-layer interaction problem that is two dimensional in the mean but with a three-component mean velocity field is studied using large-eddy simulations. The problem isolates some aspects of three-dimensionality while avoiding others and can thus offer insights into the differences between two- and three-dimensional problems. The addition of a crossflow increases the size of the separation bubble quite substantially when normalized by the boundary-layer thickness or the momentum thickness but less substantially when normalized by the displacement thickness. All cases studied are found to have a very thin precursor separation bubble before the point of true separation that extends for at least one boundary-layer thickness but remains fully within the viscous sublayer. Simulations at different Reynolds numbers show that the flow reattaches after the precursor bubble at sufficiently high Reynolds number.
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