heat transfer problem in a square cavity
Benchmark solutions for the natural convective
Ghent University, Belgium.
'Department of Flow, Heat and Combustion Mechanics,
J. Vierendeels', B. Merci' &L E. Dick'
Abstract
Rayleigh numbers.
converged results with an accuracy of 4 up to 5 digits are obtained for a variety of
pendent of grid size, grid aspect ratio, Mach number and Rayleigh number. Grid
previous work. The solver is constructed so that its convergence behaviour is inde-
is assumed. An accurate and fast multigrid solver is used, which was developed in
used and viscosity is given by Sutherland's law. A constant local Prandtl number
ber approximations of the Navier-Stokes equations are used. The ideal-gas law is
between the hot and the cold wall are large. No Boussinesq nor low-Mach num-
right and insulated on the top and bottom boundaries. The temperature differences
laminar flow of air in a square cavity which is heated on the left, cooled on the
In this study, benchmark solutions are derived for the problem of two-dimensional
1 Introduction
ied incompressible flow in a thermally driven square cavity with a pseudo-spectral
of the flow equations, simplifiedfor low-Mach number flows. Le QuCrC [3] stud-
ture differences between vertical isothermal walls. They used the transient form
[l] investigated the steady-state flow in rectangular cavities with large tempera-
function-vorticityformulationof the governing equations. Chenoweth and Paolucci
on the right and insulated on the top and bottom boundaries. They used the stream
flow of a Boussinesq fluid in a square cavity which is heated on the left, cooled
which resulted into a benchmark solution for the problem of a two-dimensional
domains with differentaspectratios. De Vahl Davis and Jones [2] presented a study
ough study for over 50 years. Most studies in the past have dealt with rectangular
Buoyancy-drivenflows,especially in two dimensions, have been the object of thor-
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Paper from: Advances in Fluid Mechanics IV, M Rahman, R Verhoeven and CA Brebbia (Editors).
ISBN 1-85312-910-0