Effect of cannelure fin configuration on compact aircooling heat sink

Applied Thermal Engineering

Volumn 31, Issue 10, 2011, Pages 1640-1647

  Wang, Chi Chuan ^a   Yang, Kai Shing ^b   Liu, Yang Ping ^c   Chen, Ing Youn ^c  

^a NATIONAL CHIAO TUNG UNIVERSITY   (Taiwan)

^b INDUSTRIAL TECHNOLOGY RESEARCH INSTITUTE   (Taiwan)

^c NATIONAL YUNLIN UNIVERSITY OF SCIENCE AND TECHNOLOGY   (Taiwan)

Author keywords

Cannelure; Dimple cavity vortex generator; Heat sink; Interrupted fin

Indexed keywords

CANNELURE; CROSS FLOWS; FIN CONFIGURATION; FRICTION REDUCTION; HEAT TRANSFER PERFORMANCE; INTERRUPTED FIN; IR IMAGES; TEST RESULTS; VORTEX GENERATORS;

INFRARED IMAGING; TEMPERATURE MEASUREMENT; TRANSPORT AIRCRAFT; VORTEX FLOW;

FINS (HEAT EXCHANGE);

EID: 79954449915     PISSN: 13594311     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.applthermaleng.2011.02.003     Document Type: Article

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