2022
DOI: 10.1177/09544089221095665
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Effect of lid height and blowing ratio on film cooling effectiveness of a novel lidded hole configuration

Abstract: Film cooling is one of the promising technologies used for protecting rocket nozzles and turbine blades from combustion chamber hot gases. This paper proposes a novel shape of film cooling injection hole, called lidded hole, that can offer significant enhancement of cooling performance. ANSYS CFX is used to perform 3D numerical simulations of a flat plate with a single row of lidded holes, in which the k–ε model approximates turbulence effects. Four cases are investigated to highlight the influence of the hole… Show more

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Cited by 2 publications
(3 citation statements)
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“… Comparison of simulated temperature distribution along the nozzle wall with experimental data from [ 26 ]. …”
Section: Figurementioning
confidence: 99%
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“… Comparison of simulated temperature distribution along the nozzle wall with experimental data from [ 26 ]. …”
Section: Figurementioning
confidence: 99%
“…The interaction of a liquid-phase film coolant and the core flow was studied numerically for a semi-cryogenic configuration by Strokach et al [ 25 ]. In a recent numerical study, Guealalia et al [ 26 ] explored the benefits of a novel approach to film injection, namely, a ‘lidded hole’ shape. The method was found to have the potential to improve cooling effectiveness significantly.…”
Section: Introductionmentioning
confidence: 99%
“…Yuen and Martinez-Botas [13,14] provided in their research papers results of heat transfer for a flat plate configuration. In order to enhance film cooling effectiveness, new hole shape of film cooling (lidded hole) was proposed in the work of Guelailia et al [15]. The effects of surface radial and longitudinal curvature on the performance of film cooling was investigated by Guelailia et al [16,17].…”
Section: Introductionmentioning
confidence: 99%