2014
DOI: 10.1016/j.ijthermalsci.2014.05.019
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An experimental investigation on transpiration cooling under supersonic condition using a nose cone model

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Cited by 50 publications
(7 citation statements)
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“…2 Associate Professor, DMS Group, PRISME Laboratory, eddy.el-tabach@univ-orleans.fr. 3 Tenure Professor, CE Group PRISME Laboratory, khaled.chetehouna@insa-cvl.fr. 4 Full Professor, CE Group, PRISME Laboratory, nicolas.gascoin@insa-cvl.fr, Senior AIAA Member.…”
Section: Cmcmentioning
confidence: 99%
See 1 more Smart Citation
“…2 Associate Professor, DMS Group, PRISME Laboratory, eddy.el-tabach@univ-orleans.fr. 3 Tenure Professor, CE Group PRISME Laboratory, khaled.chetehouna@insa-cvl.fr. 4 Full Professor, CE Group, PRISME Laboratory, nicolas.gascoin@insa-cvl.fr, Senior AIAA Member.…”
Section: Cmcmentioning
confidence: 99%
“…The Solid Oxide Fuel Cell (SOFC) for example could be used, mostly if species like hydrogen and light hydrocarbons are available onboard. In the meantime, liquid fuel (stored for propulsion application when burned in the combustion chamber) may encounter temperature that pyrolyses it and that produces light species [1][2][3][4][5] . Since the higher the H 2 or light hydrocarbons content, the longer the life time of the fuel cell, using heavy fuel would decrease the life time of the fuel cell.…”
Section: Introductionmentioning
confidence: 99%
“…Therefore, it is necessary to alleviate the cooling deterioration relating to this vapor block phenomenon by applying a new design of the transpiration cooling process. Zhao et al (2014) experimentally studied the transpiration cooling of a nose cone with unequal wall thickness. The experiment was conducted based on the arc heated supersonic free jet facility and liquid water was used as a coolant.…”
Section: Frontiers In Heat and Mass Transfermentioning
confidence: 99%
“…The coolant used and its specific capacity was the most influential parameter for the cooling efficiency. Zhao; Wang; Ma; Lin; Peng; Qu and Chen [23] presented a supersonic experimental investigation on transpiration cooling of a nose cone model with unequal thickness walled configuration using liquid water as coolant. Their experiments showed that ice cake appeared at the nose cone surface at main stream Mach number 2.0, stagnation pressure 174 kPa and mass flow rate 2.286 kg/s with an enthalpy 300 kJ/s.…”
Section: Figure 1 Scope Of Transpiration Coolingmentioning
confidence: 99%