AIAA Journal · 1996 · 15 citations · 24 references
Natural SciencesAerospace EngineeringAerodynamicsComputational Fluid DynamicsFluid DynamicsBoundary Layer FlowCompressible FlowShock WavesTurbulenceTurbulent FlowTurbulent TransportCompressible Flow ExperimentsCompressible Flow SimulationCompressible TurbulenceInstantaneous Flow VisualizationLarge-eddy StructureShock Layer StructureTurbulent Boundary LayersTurbulent Shear Flows
A countercurrent shear layer with a nominal convective Mach number (M c ) of 2 is generated using a unique arrangement. The shear layer growth rates were found to be twice that of conventional, coflowing shear layers at comparable M c . It is hypothesized that the countercurrent shear layer becomes self-excited, leading to a modification of the turbulent properties. Instantaneous flow visualization images clearly reveal the presence of large, highly convoluted, turbulent structures believed to be responsible for the enhanced growth rates. The flowfield was also examined for the presence of eddy shocklets that have been observed in numerical simulations under similar compressible flow conditions. Even though the countercurrent flowfield appears to satisfy the criteria for the creation of shocklets, a careful and thorough search revealed no evidence of their presence.
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Compressibility Effects in Turbulent Shear Layers
David W. Bogdanoff · AIAA Journal · 1983 · 562 citations