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Showing 1 to 3 of 3 for “"Compression corner"”.
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Sidewall effects in compression corner shock-wave/boundary-layer interactions
Streamwise corners are a common three-dimensional geometric feature encountered in supersonic flows, appearing in wing-body junctions, in rectangular cross sectioned inlets and research wind tunnels. When a shock wave boundary layer interaction (SBLI) occurs in a rectangular cross sectioned duct, …
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Extension to Multiple Species of a Two-Equation Turbulence Model for High Speed Flows
… step and a Mach 2.85 flow into a 24° compression corner. For the backward-facing step simulation, the surface pressure has a maximum error of 63% in the separation region, less than 5% error after the flow reattaches, and an RMS error of 17.2%, all of which are less than those of …
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Quantification of Spalart-Allmaras Turbulence Modeling Uncertainties for Hypersonic Flows Utilizing Output-Based Grid Adaptation
… areas of hypersonic geometries such as the pre-compression flat plate region and the post-compression shocked-wedge region of a compression corner. Ultimately, this study improves the determination of uncertainty bounds in engineering design involving turbulent flow, provides more insight into …