This paper discusses an adaptive grid approach, developed using Fortran 77,
on quadrilateral meshes for the Euler and Navier-Stokes solvers. Solution
adaptation is through two nonlinear heat-conduction analogies applied direc
tly on a two-dimensional surface using the finite volume method. Clustering
of the grid generated is controlled by the conductivity in the computation
al domain, which is related arbitrarily to the geometrical curvature and fl
ow gradient. Three levels of "multigrid" approach are implemented to accele
rate convergence as a grid refinement process. The grid quality is accessed
by a histogram analysis of maximum angle and aspect ratio distributions wi
thin the computational domain. This work assumes that interpolation errors
due to numerical approximation of fluxes across the surfaces of a control v
olume should become significant as the skew angle and aspect ratio increase
s. Detailed computational results and comparisons with measured data are pr
esented for steady transonic flow over a NACA0012 airfoil, supersonic flow
through a DFVLR rotor, and a 15 degrees ramp. (C) 2001 Elsevier Science Ltd
. All rights reserved.