Volume 6: Turbo Expo 2003, Parts a and B 2003
DOI: 10.1115/gt2003-38140
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Film Cooling Analysis Using DES Turbulence Model

Abstract: The complex dynamic nature of the spanwise vortices in film cooling of turbine blades makes it necessary to accurately model the flow field temporally and spatially using detailed simulation techniques like direct numerical simulation or large eddy simulation of turbulence. Although, the later requires less computational effort and thus can simulate flows at higher Reynolds number than direct simulation, both these methods remain very expensive. As a viable alternative, this paper presents a Spalart-Allamaras … Show more

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Cited by 22 publications
(6 citation statements)
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“…In designing jet engine combustors [6], unsteady reacting flow equations are solved to help reduce emission and mitigate dangerous vibrations. In designing gas turbine blades [7,8], unsteady aero and thermodynamic equations are solved to design cooling mechanisms for increased component life and overall engine efficiency. In all these applications, the unsteady equations need to be solved long enough to reproduce the chaotic, multiscale fluid dynamics.…”
Section: Introductionmentioning
confidence: 99%
“…In designing jet engine combustors [6], unsteady reacting flow equations are solved to help reduce emission and mitigate dangerous vibrations. In designing gas turbine blades [7,8], unsteady aero and thermodynamic equations are solved to design cooling mechanisms for increased component life and overall engine efficiency. In all these applications, the unsteady equations need to be solved long enough to reproduce the chaotic, multiscale fluid dynamics.…”
Section: Introductionmentioning
confidence: 99%
“…Roy et al [15] performed a flat plate film cooling analysis using a Spalart-Allamaras based detached eddy simulation (DES) approach. Their numerical model included an unstructured grid system to resolve the dynamic flow structures on both sides of the plate as well as inside the hole itself.…”
Section: Introductionmentioning
confidence: 99%
“…To capture the shear layer growth the standard LES filter scale is modified to ignore azimuthal grid spacings. Such a strategy is likely to have helped in the film cooling DES of Roy et al (2003) discussed above. Comparison is made with mean velocity and pressure profiles.…”
Section: Film Cooling Holesmentioning
confidence: 95%
“…The agreement with heat transfer measurements is encouraging. Roy et al (2003) explore the use of SA DES for film cooling. A single row of 35 • holes in a flat plate is considered.…”
Section: Film Cooling Holesmentioning
confidence: 99%