2020
DOI: 10.1016/j.applthermaleng.2020.115491
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Conjugate heat transfer of impingement cooling using conical nozzles with different schemes in a film-cooled blade leading-edge

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Cited by 27 publications
(7 citation statements)
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“…For the forced convection simulation, based on the inlet values for the fan airflow, Reynolds number is in the turbulent range (3000-12,000); therefore, the k-ε turbulence model has been used for the fluid flow and the heat transfer phenomenon. The turbulent kinetic energy k and the dissipation rate ω are obtained from the following equations [59]:…”
Section: Conjugate Convective Heat Transfer Simulationmentioning
confidence: 99%
“…For the forced convection simulation, based on the inlet values for the fan airflow, Reynolds number is in the turbulent range (3000-12,000); therefore, the k-ε turbulence model has been used for the fluid flow and the heat transfer phenomenon. The turbulent kinetic energy k and the dissipation rate ω are obtained from the following equations [59]:…”
Section: Conjugate Convective Heat Transfer Simulationmentioning
confidence: 99%
“…Another important industry in which CHT is of great interest is transportation, whether to improve the cooling of blades in aero engines [15,16], or in the automotive in-dustry either for conventional internal combustion engines [17,18] or, for example, cooling of battery packs for electrical vehicles [19].…”
Section: Introductionmentioning
confidence: 99%
“…Furthermore, as the blowing ratio increases, the benefits of using sister holes become more significant. In a few studies, FC has been used with impingement cooling to maximize coolant utilization following impingement (Immarigeon and Hassan, 2006;Liu et al, 2014;Fawzy et al, 2020;Youn et al, 2021). A real gas turbine's cooling system involves both convection and conduction heat transfer.…”
Section: Introductionmentioning
confidence: 99%
“…The study also involved varying Biot numbers (ranging from 0.013 to 3.162) to analyze their impact on the overall cooling performance. All simulations were conducted under normal temperature ranges (not actual turbine conditions) and low speeds to demonstrate conceptual designs that can be further validated through experiments (Jung et al , 2017; Nowak and Wróblewski, 2011; Panda and Prasad, 2014; Wang et al , 2015; Kazemi Kelishami and Lakzian, 2017; Fawzy et al , 2020; Singh et al , 2021a, 2021b). The temperature ratio considered for the simulations ranged from 0.67 to 0.95 (Jung et al , 2017; Jaiswal et al , 2021).…”
Section: Introductionmentioning
confidence: 99%