Numerical Analysis of the Thermal Performance of a PCM-Based Heat Sink Under Flight Random VibrationNumerical Analysis of the Thermal Performance of a PCM-Based Heat Sink Under Flight Random Vibration

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A numerical method to simulate the thermal performance of a heat sink with phase change material (PCM) under flight random vibration is presented and verified through experimental results. Constant heat flux is imposed on the heat sink in contact with paraffin wax as PCM inside a container, while the container is subjected to random vibration with the overall acceleration of 16 g rms over the frequency range of 15-2000 Hz. The enthalpy-porosity method is used to model the PCM melting process. The random vibration, defined in the frequency domain, is converted to a time signal and applied to the numerical model, which is computed in the time domain. Comparisons between the numerical and experimental results showed a good agreement, demonstrating the same heat transfer characteristics and thermal performances of the heat sink, with the average temperature difference of 0.6% for the static case and 2.2% for the vibration case.
Publisher
SPRINGER
Issue Date
2023-04
Language
English
Article Type
Article
Citation

INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.24, no.2, pp.438 - 448

ISSN
2093-274X
DOI
10.1007/s42405-022-00546-4
URI
http://hdl.handle.net/10203/306104
Appears in Collection
AE-Journal Papers(저널논문)
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