Heat transfer enhancement in a channel with rib-groove turbulators

AIP Conference Proceedings

Volumn 1207, Issue , 2010, Pages 311-316

  Kaewkohkiat, Y ^a   Kongkaitpaiboon, V ^a   Eiamsa Ard, S ^a   Pimsarn, M ^b  

^a MAHANAKORN UNIVERSITY OF TECHNOLOGY   (Thailand)

^b KING MONGKUT'S INSTITUTE OF TECHNOLOGY LADKRABANG   (Thailand)

Author keywords

Channel; Friction factor; Groove; Heat transfer; Rib; Turbulence flow

Indexed keywords

EID: 77950162830     PISSN: 0094243X     EISSN: 15517616     Source Type: Conference Proceeding    
DOI: 10.1063/1.3366383     Document Type: Conference Paper

References (4)

1. Han, J.C. and Zhang, Y.M., 1992. High performance heat transfer ducts with parallel broken and V-shaped broken ribs. Int. J. Heat Mass Transfer 35, 513-523.
2. Mochizuki, S., Murata, A. and Fukunaga, M., 1997. Effects of rib arrangements on pressure drop and heat transfer in a rib-roughened channel with a sharp 180° turn. Trans. ASME J. Turbomachinery 119, 610-616.
3. Murata, A. and Mochizuki, S., 2001. Comparison between laminar and turbulent heat transfer in a stationary square duct with transverse or angled rib turbulators. Int. J. Heat Mass Transfer 44, 1127-1141.
4. Tanda, G., 2004. Heat transfer in rectangular channel with transverse and V-shaped broken ribs. Int. J. Heat Mass Transfer 47, 229-243.