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         "type" : "Publication",
         "id"   : "https://puma.ub.uni-stuttgart.de/bibtex/283ba2e5f712d9f369456c85896362f0c/hermann",         
         "tags" : [
            "{Pin","factor;","transfer;","performance}","Friction","fins;","Heat","Thermal"
         ],
         
         "intraHash" : "83ba2e5f712d9f369456c85896362f0c",
         "interHash" : "2f4c54e29454d798df5904e114ff65b3",
         "label" : "Endwall heat transfer and pressure loss measurements in staggered arrays\n   of adiabatic pin fins",
         "user" : "hermann",
         "description" : "",
         "date" : "2017-05-18 11:32:12",
         "changeDate" : "2017-05-18 09:32:12",
         "count" : 7,
         "pub-type": "article",
         "journal": "APPLIED THERMAL ENGINEERING","publisher":"PERGAMON-ELSEVIER SCIENCE LTD","address":"THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, ENGLAND",
         "year": "{2016}", 
         "url": "", 
         
         "author": [ 
            "Meriam Axtmann","Rico Poser","Jens von Wolfersdorf","Marc Bouchez"
         ],
         "authors": [
         	
            	{"first" : "Meriam",	"last" : "Axtmann"},
            	{"first" : "Rico",	"last" : "Poser"},
            	{"first" : "Jens",	"last" : "von Wolfersdorf"},
            	{"first" : "Marc",	"last" : "Bouchez"}
         ],
         "volume": "103","pages": "1048-1056","abstract": "In many applications, pin fin arrays are used for heat transfer\n   enhancement. Due to additionally induced turbulence in the flow field,\n   the heat transfer is increased. This study focuses on different pin fin\n   arrays with thermally inactive pin fins. The configurations Include\n   short and long elements. Transient experiments are conducted to\n   determine the heat transfer characteristics on the endwall. Therefore,\n   the transient liquid crystal technique is applied to obtain locally\n   resolved heat transfer data. Three configurations with a relative\n   spacing of 2.5 <= S/D <= 5 and aspect ratio of 2 <= H/D <= 4 are\n   investigated. Hereby, the Reynolds number of the air flow, based on the\n   pin fin diameter, varies from 3 . 10(3) to 3 . 10(4). First, an overview\n   of the experimental setup and the transient measurement technique is\n   given. Then, heat transfer results on the endwall are presented in terms\n   of Nusselt number. Finally, the pressure drop is evaluated by the\n   friction factor and the thermal performance of the investigated\n   configurations is discussed. (C) 2016 Elsevier Ltd. All rights reserved.",
         "author-email" : "meriam.axtmann@itlr.uni-stuttgart.de",
         
         "issn" : "1359-4311",
         
         "keywords-plus" : "RATIO",
         
         "funding-acknowledgement" : "European Union [ACP0-GA-2010-263913]",
         
         "research-areas" : "Thermodynamics; Energy & Fuels; Engineering; Mechanics",
         
         "number-of-cited-references" : "33",
         
         "web-of-science-categories" : "Thermodynamics; Energy & Fuels; Engineering, Mechanical; Mechanics",
         
         "affiliation" : "Axtmann, M (Reprint Author), Univ Stuttgart, Inst Aerosp Thermodynam ITLR, Pfaffenwaldring 31, D-70569 Stuttgart, Germany.\n   Axtmann, Meriam; Poser, Rico; von Wolfersdorf, Jens, Univ Stuttgart, Inst Aerosp Thermodynam ITLR, Pfaffenwaldring 31, D-70569 Stuttgart, Germany.\n   Bouchez, Marc, MBDA Bourges, Aerodynam & Prop Dept, Bourges, France.",
         
         "funding-text" : "The authors would like to acknowledge the Aero-Thermodynamic Loads on\n   Lightweight Advanced Structures II project. ATLLAS II, coordinated by\n   ESA-ESTEC, is supported by the European Union within the 7th Framework\n   Programme Theme 7 Transport, Contract No.: ACP0-GA-2010-263913. Further\n   info on ATLLAS II can be found on: www.esaint/techresources/atllas\\_II",
         
         "language" : "English",
         
         "times-cited" : "0",
         
         "doi" : "10.1016/j.applthermaleng.2016.04.066",
         
         "bibtexKey": "ISI:000379560500104"

      }
	  
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