The increased demands placed presently on the performance of compressors and turbines of gas-turbine engines have, for some time, pointed the need for accurate analysis of viscous flows in turbomachinery. With the recent developments of advanced computational facilities, much effort has been made to respond to ’this need. Various mathematical formulations, grid systems and numerical techniques have been developed for the numerical solution of the viscous flow equations (Refs. 1–4). The full Navier-Stokes equations as well as their corresponding thin-layer approximate form have been employed in H- as well as C-grids, using explicit or implicit methods, including convergence enhancement techniques based on multi-grid methodology. Nevertheless, obtaining converged solutions for general geometries on acceptably refined grids remains a computationally demanding task.
[1]
U. Ghia,et al.
Study of incompressible flow separation using primitive variables
,
1981
.
[2]
J. Bennett,et al.
Statistical characteristics of velocity, concentration, mass transport, and momentum transport for coaxial jet mixing in a confined duct
,
1983
.
[3]
S. J. Shamroth,et al.
Prediction of cascade flow fields using the averaged Navier-Stokes equations
,
1984
.
[4]
G. M. Johnson,et al.
Efficient solution of the Euler and Navier-Stokes equations with a vectorized multiple-grid algorithm
,
1983
.