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
Link To Document :
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