Abstract
The effect of the cavity depth on the leakage flow and tip cooling has been numerically investigated in a honeycomb-tip turbine cascade with cooling injection. Coolant is ejected through the center holes on the honeycomb cavity bottoms. Three dimensional flow fields were simulated using the Reynolds-averaged Navier-Stokes (RANS) method and the k-ω turbulence model. Then the tip configurations are evaluated according to several performance parameters, such as leakage mass flow rate, total pressure loss and film cooling effectiveness, in the upper passage, the gap and the honeycomb cavities. Furthermore, the secondary velocity streamlines are plotted at the cascade exit to characterize the upper passage vortices. The isothermal surface and contours of dimensional temperature are presented to explore the mixing between the coolant and the cavity vortices. The numerical results show that the aerodynamic and thermodynamic performance differs significantly with the cavity depth.
Published Version
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