Please use this identifier to cite or link to this item: http://bura.brunel.ac.uk/handle/2438/9082
Title: Tests of prototype PCM 'sails' for office cooling
Authors: Susman, G
Dehouche, Z
Cheechern, T
Craig, S
Keywords: Buildings;Cooling;PCM;Sails;Energy;Enthalpy-porosity model
Issue Date: 2011
Publisher: Elsevier
Citation: Applied Thermal Engineering, 31(5), 717 - 726, 2011
Abstract: PCM modules, constructed from a paraffin/LDPE composite, were tested in an occupied London office, in summer. Design variations tested the effect on heat transfer of a black paint or aluminium surface, the effect of different phase transition zones and the effect of discharging heat inside or outside. The modules’ temperatures were monitored along with airflow rate, air temperature and globe temperature. Their small size meant any effect on room temperature was negligible. Using DSC measurements of the PCMs’ thermophysical properties, in conjunction with the environmental measurements, a semi-empirical model of the modules was constructed in FLUENT using an enthalpy-porosity formulation to model phase change. Good validation was obtained for all modules using the temperature measurements with notable divergence when maximum liquid fraction was reached. The model was validated by the temperature measurements and used to generate mean liquid fraction and surface heat transfer rate profiles for performance comparisons. The broad phase transition zones of the PCMs results in wasted latent heat capacity. Black modules transfer heat and exhaust latent storage capacity significantly quicker than aluminium modules, due to radiant exchange. Discharging heat outside leads to an increase in thermal storage capacity and a higher rate of heat absorption.
Description: This is the post-print version of the final paper published in Applied Thermal Engineering. The published article is available from the link below. Changes resulting from the publishing process, such as peer review, editing, corrections, structural formatting, and other quality control mechanisms may not be reflected in this document. Changes may have been made to this work since it was submitted for publication. Copyright @ 2010 Elsevier B.V.
URI: http://www.sciencedirect.com/science/article/pii/S1359431110004357
http://bura.brunel.ac.uk/handle/2438/9082
DOI: http://dx.doi.org/10.1016/j.applthermaleng.2010.10.008
ISSN: 1359-4311
Appears in Collections:Mechanical and Aerospace Engineering
Dept of Mechanical Aerospace and Civil Engineering Research Papers

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