Nazmiye Açıkgöz
M. S., Department of Aeronautical Engineering
Supervisor: Assoc. Prof. Dr. İsmail Hakkı Tuncer
January 2001, 78 Pages
ABSTRACT
Navier-Stokes solutions are obtained for unsteady multi-passage cascade
flows with Baldwin-Lomax, Baldwin-Barth, Spalart-Allmaras and k-w turbulence
models. The full multi-passage flow domain with periodic boundaries is
discretized with overset grids. Computations are carried out in parallel
using Parallel Virtual Machine (PVM) library routines. The performance
of the turbulence models is assessed for three different cases, a single
element airfoil, a compressor cascade (MTU) and a turbine cascade (STC4).
Comparisons of different flow variables and turbulence quantities are carried
out. It is concluded that the turbulence models do not affect steady and
unsteady cascade flows significantly for the flow cases studied.
Keywords: Turbulence Modelling, Cascade Flow, Overset Grids, Eddy viscosity, Parallel Processing, PVM, Plunge, Reynolds-Averaged Navier Stokes Equations, Finite Difference Method.
Abstract in Turkish |
Thesis Presentation |