Customer Login Shopping Cart
Library Subscription: Guest
Home Archives Officers Future meetings Indian Society for Heat and Mass Transfer

ISSN Online: 2688-7231

ISBN Online: 978-1-56700-524-0

Proceedings of the 26thNational and 4th International ISHMT-ASTFE Heat and Mass Transfer Conference December 17-20, 2021, IIT Madras, Chennai-600036, Tamil Nadu, India
December, 17-20, 2021, IIT Madras, Chennai, India

Numerical Investigation on Heat Transfer Coefficient of Supercritical CO2 in a extended surface Micro Heat-sink

Get access DOI: 10.1615/IHMTC-2021.1250
pages 835-840

Abstract

Due to the conventional cooling system limitations, miniaturization of electronic components have necessitated researchers to explore substitute working fluids and miniscale components to enhance heat transfer efficiency. Also, this immense increase in heat generation necessitated researchers to search for an alternate coolant with enhanced heat removal capabilities. In particular, supercritical CO2 has been identified as next generation coolant owing to its realizable working condition and environment friendly characteristics. In this study, flow and thermal behavior of micro heat-sinks with micro-fins were investigated considering supercritical carbon dioxide as working fluid. In addition to plane microchannel, an extended surface namely NACA-6412 airfoil has been included in the present study. CFD analysis is performed to assess the influence of micro-fins, mass flux on flow and thermal behavior of turbulent supercritical carbon dioxide flow for P = 80 bar, q'" = 40 - 100 kW/m2, G = 400 - 1000 kg/m2s, Tin = 305 - 320 K. The results showed that finned microchannels showed enhanced heat transfer coefficient due to higher surface area and disruption in flow field. Moreover, finned microchannel resulted in lower wall temperature compared to plane microchannel. For finned microchannel heat sink, higher mass flux demonstrated heat transfer enhancement.
Home Archives Officers Future meetings Indian Society for Heat and Mass Transfer English Русский 中文 Português Help Contact Us Back to ISHMT