Numerical simulation of tip leakage flows in axial flow turbines, with emphasis on flow physics: Part I - Effect of tip clearance height

A pressure correction based, 3D Navier-Stokes CFD code was used to simulate the effects of turbine parameters on the tip leakage flow and vortex in a linear turbine cascade to understand the detailed flow physics. A baseline case simulation of a cascade was first conducted in order to validate the n umerical procedure with experimental measurements. The effects of realistic tip clearance spacing, inlet conditions, and relative endwall motion were then sequentially simulated, while maintaining previously modified paramete rs. With each additional simulation, a detailed comparison of the leakage f low's direction, pressure gradient, and mass flow, as well as the leakage v ortex and its roll-up, size, losses, location, and interaction with other f low features, was conducted. Part I of this two-part paper focuses on the e ffect of reduced tip clearance height on the leakage flow and vortex. Reduc ed tip clearance results in less mass flow through the gap, a smaller leaka ge vortex, and less aerothermal losses in both the gap and the vortex. The shearing of the leakage jet and passage flow to which leakage vortex roll-u p is usually attributed to is not observed in any of the simulations. Alter native explanations of the leakage vortex's roll-up are presented. Addition al secondary flows that are seen near the casing are also discussed.