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Showing 1 to 2 of 2 for “"Gas turbine aerodynamics"”.
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Computational Investigation of Perforated Plate Film Cooling Utilizing Conjugate Heat Transfer
<p>The accuracy of modern state-of-practice computational fluid dynamics approaches in predicting the cooling effectiveness of a perforated plate film-cooling arrangement is evaluated in ANSYS Fluent. A numerical investigation is performed using the Reynolds Averaged Navier Stokes equations and …
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The relationship between surface geometry and transonic intake performance during off-design climb
The design of slimmer, shorter gas-turbine nacelles supports lower emissions in civil aviation. However, these designs often have a stronger shock on the windward front-lip of the intake during off-design climb, producing a severe shock wave--boundary-layer interaction (SBLI) that greatly increases …