LAPSE:2023.33012
Published Article

LAPSE:2023.33012
Effect of Mainstream Velocity on the Optimization of a Fan-Shaped Film-Cooling Hole on a Flat Plate
April 20, 2023
Abstract
In this study, the effect of mainstream velocity on the optimization of a fan-shaped hole on a flat plate was experimentally investigated. The experiment was conducted by changing the forward expansion angle (βfwd), lateral expansion angle (βlat), and metering length ratio (Lm/D) of the film-cooling hole. A total of 13 cases extracted using the Box−Behnken method were considered to examine the effect of the shape parameters of the film-cooling hole under a 90 m/s mainstream velocity condition, and the results were compared with the results derived under a mainstream velocity of 20 m/s. One density ratio (DR = 2.0) and a blowing ratio (M) ranging from 1.0 to 2.5 were considered, and the pressure-sensitive paint (PSP) technique was applied for the film-cooling effectiveness (FCE). As a result of the experiment, the optimized hole showed a 49.3% improvement in the overall averaged FCE compared to the reference hole with DR = 2.0 and M = 2.0. As the blowing ratio increased, the hole exit area tended to increase, and this tendency was the same as that in the 20 m/s mainstream condition.
In this study, the effect of mainstream velocity on the optimization of a fan-shaped hole on a flat plate was experimentally investigated. The experiment was conducted by changing the forward expansion angle (βfwd), lateral expansion angle (βlat), and metering length ratio (Lm/D) of the film-cooling hole. A total of 13 cases extracted using the Box−Behnken method were considered to examine the effect of the shape parameters of the film-cooling hole under a 90 m/s mainstream velocity condition, and the results were compared with the results derived under a mainstream velocity of 20 m/s. One density ratio (DR = 2.0) and a blowing ratio (M) ranging from 1.0 to 2.5 were considered, and the pressure-sensitive paint (PSP) technique was applied for the film-cooling effectiveness (FCE). As a result of the experiment, the optimized hole showed a 49.3% improvement in the overall averaged FCE compared to the reference hole with DR = 2.0 and M = 2.0. As the blowing ratio increased, the hole exit area tended to increase, and this tendency was the same as that in the 20 m/s mainstream condition.
Record ID
Keywords
fan-shaped hole, film cooling, gas turbine, shape optimization
Subject
Suggested Citation
Lee SI, Jung JY, Song YJ, Kwak JS. Effect of Mainstream Velocity on the Optimization of a Fan-Shaped Film-Cooling Hole on a Flat Plate. (2023). LAPSE:2023.33012
Author Affiliations
Lee SI: School of Aerospace and Mechanical Engineering, Korea Aerospace University, Goyang 10540, Korea
Jung JY: School of Aerospace and Mechanical Engineering, Korea Aerospace University, Goyang 10540, Korea
Song YJ: School of Aerospace and Mechanical Engineering, Korea Aerospace University, Goyang 10540, Korea
Kwak JS: School of Aerospace and Mechanical Engineering, Korea Aerospace University, Goyang 10540, Korea [ORCID]
Jung JY: School of Aerospace and Mechanical Engineering, Korea Aerospace University, Goyang 10540, Korea
Song YJ: School of Aerospace and Mechanical Engineering, Korea Aerospace University, Goyang 10540, Korea
Kwak JS: School of Aerospace and Mechanical Engineering, Korea Aerospace University, Goyang 10540, Korea [ORCID]
Journal Name
Energies
Volume
14
Issue
12
First Page
3573
Year
2021
Publication Date
2021-06-16
ISSN
1996-1073
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Original Submission
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PII: en14123573, Publication Type: Journal Article
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LAPSE:2023.33012
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https://doi.org/10.3390/en14123573
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Apr 20, 2023
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