Analysis of unsteady supersonic cavity flow employing an adaptive meshing algorithm
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Publication:2564658
DOI10.1016/0045-7930(95)00045-3zbMath0888.76063OpenAlexW2074897613MaRDI QIDQ2564658
Publication date: 11 June 1998
Published in: Computers and Fluids (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/0045-7930(95)00045-3
Reynolds-averaged Navier-Stokes equationstime scaleRiemann solverlength scalecompressibility corrections\(k\)-\(\omega\) turbulence model
Finite difference methods applied to problems in fluid mechanics (76M20) Shear flows and turbulence (76F10) Supersonic flows (76J20)
Related Items (1)
Cites Work
- Adaptive mesh refinement for hyperbolic partial differential equations
- Approximate Riemann solvers, parameter vectors, and difference schemes
- A parallel adaptive grid algorithm for computational shock hydrodynamics
- Riemann Solvers, the Entropy Condition, and Difference
- Reassessment of the scale-determining equation for advanced turbulence models
- Numerical simulation of supersonic flow over a three-dimensional cavity
- Analyses of Pressure Oscillations in an Open Cavity
- Dilatation-dissipation corrections for advanced turbulence models
- Turbulence models for compressible boundary layers
- Compressible cavity flow oscillation due to shear layer instabilities and pressure feedback
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