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NASA NTRS · 19950044885

Multigrid solution of compressible turbulent flow on unstructured meshes using a two-equation model

Abstract

The steady state solution of the system of equations consisting of the full Navier-Stokes equations and two turbulence equations has been obtained using a multigrid strategy of unstructured meshes. The flow equations and turbulence equations are solved in a loosely coupled manner. The flow equations are advanced in time using a multistage Runge-Kutta time-stepping scheme with a stability-bound local time step, while turbulence equations are advanced in a point-implicit scheme with a time step which guarantees stability and positivity. Low-Reynolds-number modifications to the original two-equation model are incorporated in a manner which results in well-behaved equations for arbitrarily small wall distances. A variety of aerodynamic flows are solved, initializing all quantities with uniform freestream values. Rapid and uniform convergence rates for the flow and turbulence equations are observed.

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BibTeXRIS

Mavriplis, D. J., Matinelli, L.. 1994-05-01. Multigrid solution of compressible turbulent flow on unstructured meshes using a two-equation model. https://ntrs.nasa.gov/citations/19950044885

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