
doi: 10.2514/3.12808
A staggered finite volume upwind algorithm for solving the compressible Navier-Stokes equations and the \(k-\omega\) turbulence model equations has been developed for computing cascade flows. Roe's upwind scheme is used to discretize the convective terms of the Navier-Stokes equations, and a third-order upwind scheme is used for the convective terms of the \(k-\omega\) equations. All of the diffusion terms are discretized with the central-difference method. By the use of a combination of cell-centered and cell-vertex schemes, the method maintains a small stencil for all of the diffusion terms and makes the Navier-Stokes equations and \(k-\omega\) equations strongly coupled. The algorithm was tested for a flat-plate flow, a supersonic wedge cascade flow, and a low-pressure turbine cascade flow at design and off-design conditions.
shock capturing, Other numerical methods (fluid mechanics), separation prediction, Roe's upwind scheme, supersonic wedge cascade flow, Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics, cell-vertex schemes, flat-plate flow, central-difference method, finite volume algorithm, Shear flows and turbulence, third-order upwind scheme, low-pressure turbine cascade flow
shock capturing, Other numerical methods (fluid mechanics), separation prediction, Roe's upwind scheme, supersonic wedge cascade flow, Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics, cell-vertex schemes, flat-plate flow, central-difference method, finite volume algorithm, Shear flows and turbulence, third-order upwind scheme, low-pressure turbine cascade flow
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