Computation of the turbulent flow field around an aerofoil by k‐ϵ‐γ model in a non‐staggered, C‐type single‐grid system
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Publication:4858242
DOI10.1002/CNM.1640111102zbMath0836.76072OpenAlexW2081180869MaRDI QIDQ4858242
Publication date: 1 February 1996
Published in: Communications in Numerical Methods in Engineering (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1002/cnm.1640111102
numerical instabilityvelocity-pressure couplingbranch-cuttwo-dimensional aerofoilnon- staggered finite volume method
Cites Work
- A low dispersion and bounded convection scheme
- The numerical computation of turbulent flows
- Numerical study of the turbulent flow past an airfoil with trailing edge separation
- A closure model for conditioned stress equations and its application to turbulent shear flows
- USE OF A PRESSURE-WEIGHTED INTERPOLATION METHOD FOR THE SOLUTION OF THE INCOMPRESSIBLE NAVIER-STOKES EQUATIONS ON A NONSTAGGERED GRID SYSTEM
- AK—ε—γ equation turbulence model
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