2017
DOI: 10.1016/j.applthermaleng.2017.06.031
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Heat transfer enhancement of perforated pin heat sink in future aircraft applications

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Cited by 27 publications
(7 citation statements)
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“…Sakanova [21] studied the 3D conjugate heat transfer in perforated heat sink under aerospace conditions. Liquid and gas coolant such as water, oil, fuel, and air was used under laminar and turbulent conditions.…”
Section: Authors Flow Conditions and Geometry Study Resultsmentioning
confidence: 99%
“…Sakanova [21] studied the 3D conjugate heat transfer in perforated heat sink under aerospace conditions. Liquid and gas coolant such as water, oil, fuel, and air was used under laminar and turbulent conditions.…”
Section: Authors Flow Conditions and Geometry Study Resultsmentioning
confidence: 99%
“…Hydrofoil shape has the conic arc with shape parameter of 0.5. Thermo-physical properties of fuel and air is taken from [2]. The inlet velocity for each type of flow is presented in Table 2.…”
Section: Methodsmentioning
confidence: 99%
“…Pin fin heat sink seems to be promising for aircraft cooling system. The latest work of the same group [2] deal with the heat transfer enhancement by applying the perforated pin fin heat sink for cooling system in future aircraft. It is concluded that perforation can not only improve the heat transfer but also results in weight reduction.…”
Section: Introductionmentioning
confidence: 99%
“…The results showed that for an optimal range of porosities at a specified perforation range, the laterally perforated finned heat sink has a lower thermal resistance at a constant pumping power through the heat sink base. Sakanova 40 worked on augmentation of heat transfer through perforated finned heat sink for aircraft. The outcome of this study showed that when air is used, the rate of heat transfer of perforated finned heat sink is found to be greater than solid pin‐fin geometry for laminar as well as turbulent flow.…”
Section: Experimental Studiesmentioning
confidence: 99%