Effect of attack angle and jet height on impingement and film composite cooling of turbine blade leading edge

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dc.contributor.authorLiu, Zhao
dc.contributor.authorYe, Lv
dc.contributor.authorYang, Xing
dc.contributor.authorFeng, Zhenpingen_US
dc.contributor.otherInternational Society for Air Breathing Engines
dc.date.accessioned2015-10-22T15:51:15Z
dc.date.available2015-10-22T15:51:15Z
dc.date.created2015en_US
dc.date.issued2015-10-22
dc.descriptionThis paper is part of the conference proceedings from the 22nd International Symposium on Air Breathing Engines.en_US
dc.identifier20109en_US
dc.identifier.urihttp://hdl.handle.net/2374.UC/745710
dc.relation.ispartofISABE 2015 (Awatef Hamed, Faculty Work and Research, College of Engineering and Applied Science)en_US
dc.rightsAttribution-NonCommercial-NoDerivs 3.0 United Statesen_US
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/3.0/us/en_US
dc.subjectThermal management: Cooling technologyen_US
dc.subject.lcshAirplanes -- Motorsen_US
dc.subject.lcshAirplanes -- Jet propulsionen_US
dc.subject.lcshAircraft gas-turbinesen_US
dc.titleEffect of attack angle and jet height on impingement and film composite cooling of turbine blade leading edgeen_US
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