Analysis of unsteady supersonic cavity flow employing an adaptive meshing algorithm (Q2564658)
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| English | Analysis of unsteady supersonic cavity flow employing an adaptive meshing algorithm |
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Analysis of unsteady supersonic cavity flow employing an adaptive meshing algorithm (English)
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11 June 1998
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We present numerical analysis of a supersonic cavity flow, including the effects of length scale, computational grid and time scale. A turbulent flow over a two-dimensional cavity has been analyzed through solutions of the Reynolds-averaged Navier-Stokes equations. The effects of turbulence were modelled through a coupled solution of a \(k\)-\(\omega\) turbulence model using compressibility corrections. A Riemann solver was employed, and an adaptive mesh refinement technique has been used to capture the features of the transient fluid flow.
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\(k\)-\(\omega\) turbulence model
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length scale
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time scale
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Reynolds-averaged Navier-Stokes equations
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compressibility corrections
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Riemann solver
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