4.7 Article

Experimental investigation of supercritical carbon dioxide in horizontal microchannels with non-uniform heat flux boundary conditions

期刊

出版社

PERGAMON-ELSEVIER SCIENCE LTD
DOI: 10.1016/j.ijheatmasstransfer.2018.10.027

关键词

Microchannel; Heat transfer; Supercritical; Carbon dioxide; Experimental; Non-uniform heat flux; Buoyancy; Flow acceleration

资金

  1. National Science Foundation [1604433]
  2. Directorate For Engineering
  3. Div Of Chem, Bioeng, Env, & Transp Sys [1604433] Funding Source: National Science Foundation

向作者/读者索取更多资源

Supercritical carbon dioxide (sCO(2)) experiences a drastic change in its thermophysical properties near the thermodynamic critical point. A non-linear thermophysical property variation can influence the heat transfer behavior of sCO(2) which is not predicted well by conventional single phase heat transfer theory. This can become a major hindrance in the effective design of heat exchangers using sCO(2) as a heat transfer fluid and operating in the vicinity of the critical point. Previous investigations of sCO(2) heating have been primarily focused on macroscale, circular and uniformly heated channels at relatively low heat fluxes. It is unclear if models and correlations developed from large circular tube data can be scaled down to the microscale, non-circular channels subject to non-uniform heating. The present study experimentally investigates the turbulent heat transfer performance of sCO(2) in a microchannel heat exchanger operating in a horizontal configuration with a single wall non-uniform heat flux boundary condition. The test section has five parallel channels with a 0.75 mm hydraulic diameter and an aspect ratio of 1. The channels are fabricated using computer numerical control machining and the test section sealed using a diffusion bonding approach. Data analysis techniques which employ 2-D and 3-D heat transfer models of the experimental test section are developed to calculate the average heat transfer coefficients for a given set of experimental conditions. Data are obtained over a wide range of experimental parameters including test section applied heat flux (20 <= q '' <= 40W cm(-2)), mass flux (500 <= G <= 1000 kg m(-2) s(-1)), reduced pressure (1.03 <= P-R <= 1.1), and inlet temperatures (16 <= T-in <= 50 degrees C). The heat transfer data were screened for the presence of buoyancy and flow acceleration effects and then compared against correlations developed for turbulent subcritical and supercritical fluid flows. (C) 2018 Elsevier Ltd. All rights reserved.

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