A numerical investigation study was performed to study the phase change behavior of wax/foam composite encapsulated in an aluminum casing. Two types of foam materials, namely, aluminum and carbon, were infiltrated with paraffin wax. The progress of melt interface and temperature distribution within the encapsulated composite was analyzed using computational fluid dynamics software (CFD). A two-energy equation model was implemented in the CFD software through the use of user defined function (UDF). Interfacial effects influencing the heat transfer process at the casing-composite junction and between the wax-foam surfaces within the composite were addressed through the use of separate UDF. In addition, the effect of capillary pressure developed within the foam matrix was incorporated using an area ratio parameter. The contact resistance at the foam-casing interface and the capillary pressure had a major influence on the thermal behavior of the system. These two factors lowered down the heat transfer rate considerably and the melting area was reduced by more than 30%. The temperature profiles for the foam material showed a different pattern as compared to the temperature within the wax, which was due to the effect of thermal nonequilibrium.
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1 August 2007
Research Article|
August 06 2007
Interfacial and capillary pressure effects on the thermal performance of wax/foam composites
M. Almajali;
M. Almajali
a)
University of Dayton
, 300 College Park, Dayton, Ohio 45469
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K. Lafdi;
K. Lafdi
University of Dayton
, 300 College Park, Dayton, Ohio 45469
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S. Shaikh
S. Shaikh
University of Dayton
, 300 College Park, Dayton, Ohio 45469
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a)
Author to whom correspondence should be addressed; electronic mail: almajamr@notes.udayton.edu
J. Appl. Phys. 102, 033506 (2007)
Article history
Received:
March 30 2007
Accepted:
June 21 2007
Citation
M. Almajali, K. Lafdi, S. Shaikh; Interfacial and capillary pressure effects on the thermal performance of wax/foam composites. J. Appl. Phys. 1 August 2007; 102 (3): 033506. https://doi.org/10.1063/1.2767268
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