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Journal ArticleDOI

Numerical analysis of microholes film/effusion cooling effectiveness

Tomasz Ochrymiuk
- 09 Sep 2017 - 
- Vol. 26, Iss: 5, pp 459-464
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TLDR
In this article, numerical simulations were performed to predict the film cooling effectiveness on the fiat plate with a three-dimensional discrete hole film cooling RSM-AKN turbulent heat transfer models based on variable turbulent Prandtl number approaches were considered.
Abstract
Numerical simulations were performed to predict the film cooling effectiveness on the fiat plate with a three-dimensional discrete hole film cooling RSM-AKN turbulent heat transfer models based on variable turbulent Prandtl number approaches were considered. Obtained numerical results were directly compared with the data that came from an experiment based on Transient Liquid Crystal methodology. All implemented models for turbulent heat transfer performed sufficiently well for the considered case. It was confirmed, however, that the two-equation closure can give a detailed look into film cooling problems without using any time-consuming and inherently unsteady models. The RSM-AKN turbulent model was used in micoholes case too. The main target of simulations was maintain the same level of cooling efficiency ratio in both cases and confirm that is possible significantly reduce mass flows of the coolant in microholes case.

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References
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Turbulent Prandtl number : where are we ?

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Gas Turbine Heat Transfer: Ten Remaining Hot Gas Path Challenges

TL;DR: In this paper, the authors identify ten major thermal issues for the turbine hot gas path (HGP) today, including uniformity of internal cooling, ultimate film cooling, micro-cooling, reduced incident heat flux, secondary flows as prime cooling, contoured gas paths, thermal stress reduction, controlled cooling, low emission combustor-turbine systems, and regenerative cooling.
Journal ArticleDOI

Numerical modelling of film cooling from converging slot-hole

TL;DR: In this article, the authors presented a numerical prediction of a new 3D film cooling hole geometry, the converging slot-hole or console, which is designed in order to improve the heat transfer and aerodynamic loss performance of turbine vane and rotor blade cooling systems without loosing the mechanical strength of a row of discrete holes.
Journal ArticleDOI

Film cooling at hypersonic Mach numbers using forward facing array of micro-jets

TL;DR: In this paper, a single jet and an array of micro-jets are injected from the stagnation zone of a blunt cone model (58, apex angle and nose radius of 35 mm). Nitrogen and Helium are injected as coolant gases.
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