4.3 Article

Computational and Experimental Study of Film-Cooling Effectiveness With and Without Downstream Vortex Generators

Journal

Publisher

ASME
DOI: 10.1115/1.4055529

Keywords

vortex generators; gas-turbine heat transfer; film cooling effectiveness; aerothermal test facility; conjugate heat transfer

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This study investigates the effect of downstream vortex generators on film cooling effectiveness through computational and experimental methods. The computational study is based on steady RANS equations closed by the SST turbulence model with and without conjugate heat transfer analysis. The experimental study is conducted using a conjugate heat transfer test rig, measuring velocity and temperature profiles upstream and downstream of the film-cooling holes, as well as temperature at various locations on the film-cooled flat plate. The results show the influence of blowing ratio and temperature ratio on flow structures and film cooling effectiveness.
Downstream vortex generators that involve a pair of rectangular plates arranged in an open V-shape placed just downstream of each film-cooling hole were shown to create flow and vortical structures that entrain lifted film-cooling flow back to the surface and increase its lateral spreading on the surface (GT2020-14317). In this study, computations and measurements were performed to examine the flow mechanisms this vortex generator induces to improve film-cooling effectiveness of a flat plate with the cooling flow emanating from one row of inclined holes. Parameters studied include blowing ratio (BR = 0.75 and 1.0) and temperature ratio (TR = 1.07 and 1.9). The computational study is based on steady Reynolds-averaged Navier-Stokes (RANS) closed by the shear-stress transport (SST) turbulence model with and without conjugate analysis. The experimental study was conducted by using a conjugate heat transfer test rig with a plenum, where cooling flow is introduced. Measurements made include velocity and temperature profiles upstream and downstream of the film-cooling holes as well as the temperature at several locations on the hot and cold sides of the film-cooled flat plate. The computational study was validated by comparing computed results with those from measurements at BR = 0.75 and 1.0 and TR = 1.9. Computational and experimental results are presented to show the effects of BR and TR on the flow structures and how those structures improve the effectiveness of film cooling with and without the downstream vortex generators and with and without conjugate heat transfer.

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