Title of article
An approximate methodology to simulate combined conduction-radiation heat transfer for multi-layer insulator
Author/Authors
Torabi, A. Aerospace Research Institute (Ministry of Science -Research and Technology) - 14665-834, Tehran, Iran - Department of Aerospace Engineering - Sharif University of Technology - Tehran, P.O. Box 11365-11155, Iran , Abedian, A. Department of Aerospace Engineering - Sharif University of Technology - Tehran, P.O. Box 11365-11155, Iran , Farsi, M.A. Aerospace Research Institute (Ministry of Science -Research and Technology) - 14665-834, Tehran, Iran
Pages
9
From page
2924
To page
2932
Abstract
A quasi-analytical methodology was developed to model combined conductionradiation
heat transfer through the thickness of a re ective multi-layer insulator. This
methodology was validated based on the experimental result. It can be applied to the
initial design of high-temperature multi-layer insulators. Traditionally, radiation thermal
conductivity approximation was employed for the initial stages of design. Despite the acceptable
accuracy of this approach in steady state cases, it yields some unacceptable errors
when thermal load is transient. It was shown that the older version of this methodology
could not predict maximum temperature and time of occurrences by acceptable margins.
The developed model originated from the radiation thermal conductivity approximation.
Unlike the primitive one, the developed model shows acceptable performance in transient
cases. This model was developed with emphasis on thermal emittance through the thickness
of the insulator. It can predict the maximum temperature of a structure and its occurrence
time with an error less than 4%.
Keywords
Combined conductionradiation , Re ective multi-layer insulator , Approximate methodology , Eective thermal conductivity , Absorption area
Journal title
Scientia Iranica(Transactions B:Mechanical Engineering)
Serial Year
2020
Record number
2573644
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