Film cooling effectiveness of a single row of cylindrical holes on a flat plate was analyzed. It was found, that the flow can be divided into two typical regimes along the downstream distance. Near the ejection location a complex flow domain of cooling film formation with strong 3-D character was recognized. Further downstream a domain of a diluting cooling film with 2-D character was identified. An analytical solution for the film cooling effectiveness along the downstream distance was derived in the 2-D regime. Based on literature data, correlations for the formation length, i.e. the length of the 3-D domain, and the corresponding film cooling effectiveness at the start of the 2-D film were developed. These correlations provide the initial conditions of the analytical solution of the 2-D film flow. A damping function was introduced to connect the two regimes and to model the lateral averaged film cooling effectiveness distribution within the 3-D flow domain. From this, a correlation was established, taking into account the full set of parameters, which was presented in an earlier study [1]. The correlation was tested over a wide range of parameters, and an error estimation is given to demonstrate the quality of the correlation.
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ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition
June 2–5, 1997
Orlando, Florida, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7870-5
PROCEEDINGS PAPER
An Overall Correlation of Film Cooling Effectiveness From One Row of Holes
Michael Scheurlen
Michael Scheurlen
Siemens AG/KWU, Mülheim/Ruhr, Germany
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S. Baldauf
Universität Karlsruhe, Germany
A. Schulz
Universität Karlsruhe, Germany
S. Wittig
Universität Karlsruhe, Germany
Michael Scheurlen
Siemens AG/KWU, Mülheim/Ruhr, Germany
Paper No:
97-GT-079, V003T09A010; 8 pages
Published Online:
December 24, 2014
Citation
Baldauf, S, Schulz, A, Wittig, S, & Scheurlen, M. "An Overall Correlation of Film Cooling Effectiveness From One Row of Holes." Proceedings of the ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition. Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration. Orlando, Florida, USA. June 2–5, 1997. V003T09A010. ASME. https://doi.org/10.1115/97-GT-079
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