2021
DOI: 10.3390/aerospace8050128
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Effect of Two-Head Flared Hole on Film Cooling Performance over a Flat Plate

Abstract: Film cooling is commonly utilized in turbine blades to decrease the temperature of the air stream from the combustion chamber that contacts directly with the blades. The shape of a cylindrical hole (CH) with the geometrical variations at inlet and outlet ports was examined using the 3D Reynolds-averaged Navier–Stokes equations (RANS) with a shear stress transport (SST k − ω) turbulence model to study the effect of the two-head flared hole on film cooling effectiveness (FE) at high accuracy with a small y+ valu… Show more

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Cited by 3 publications
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