Multislope MUSCL method for unstructured meshes applied to the compressible axisymmetric Euler equations for swirling flows
Journal of Computational Physics, Jul 1, 2010
A finite volume method for the numerical solution of axisymmetric inviscid swirling flows
is pre... more A finite volume method for the numerical solution of axisymmetric inviscid swirling flows
is presented. The governing equations of the flow are the axisymmetric compressible Euler
equations including swirl (or tangential) velocity. A first-order scheme is introduced where
the convective fluxes at cell interfaces are evaluated by the Rusanov or the HLLC numerical
flux while the geometric source terms are discretizated to provide a well-balanced scheme
i.e. the steady-state solutions with null velocity are preserved. Extension to the secondorder
space approximation using a multislope MUSCL method is then derived. To test
the numerical scheme, a stationary solution of the fluid flow following the radial direction
has been established with a zero and nonzero tangential velocity. Numerical and exact
solutions are compared for classical Riemann problems where we employ different limiters
and effectiveness of the multislope MUSCL scheme is demonstrated for strongly shocked
axially symmetric flows like in spherical bubble compression problem. Two other tests
with axisymmetric geometries are performed: the supersonic flow in a tube with a cone
and the axisymmetric blunt body with a free stream.
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Papers by D. Rochette
is presented. The governing equations of the flow are the axisymmetric compressible Euler
equations including swirl (or tangential) velocity. A first-order scheme is introduced where
the convective fluxes at cell interfaces are evaluated by the Rusanov or the HLLC numerical
flux while the geometric source terms are discretizated to provide a well-balanced scheme
i.e. the steady-state solutions with null velocity are preserved. Extension to the secondorder
space approximation using a multislope MUSCL method is then derived. To test
the numerical scheme, a stationary solution of the fluid flow following the radial direction
has been established with a zero and nonzero tangential velocity. Numerical and exact
solutions are compared for classical Riemann problems where we employ different limiters
and effectiveness of the multislope MUSCL scheme is demonstrated for strongly shocked
axially symmetric flows like in spherical bubble compression problem. Two other tests
with axisymmetric geometries are performed: the supersonic flow in a tube with a cone
and the axisymmetric blunt body with a free stream.