top of page
Turbomachinery
F.S. Lien and M.A. Leschziner (1999), “Computational Modelling of a Transitional 3D Turbine-Cascade Flow Using a Modified Low-Re k-e Model and a Multi-Block Scheme”, Int. J. of Computational Fluid Dynamics, Vol. 12, pp. 1-15.
-
Expt. by Gregory-Smith & Cleak (1992)
-
Multi-block grid containing 725,000 nodes
-
Low-Re k-e model of Lien & Leschziner (1995)
-
Inlet flow angle: 42.75 degrees



bottom of page