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Numerical Investigation of a Corrugated Heat Source Cavity: A Full Convection-Conduction-Radiation Coupling

Received: 14 November 2017     Accepted: 27 November 2017     Published: 3 January 2018
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Abstract

In present study a numerical analysis of complex heat transfer (turbulent natural convection, conduction and surface thermal radiation) in a rectangular enclosure with a heat source has been carried out. The finite volume method based on SIMPLEC algorithm has been utilized. The effects of Rayleigh number in a range from 108 to 1011, internal surface emissivity 0≤ε˂1 on the fluid flow and heat transfer have been extensively explored. Detailed results including temperature fields, flow profiles, and average Nusselt numbers have been presented. In this investigation it has been tried to study the shape of heat source influence on heat transfer and fluid field in the considered domain. According to results in low emissivity values usage of circular obstacles is recommended. Although in high emissivity values using rectangular obstacles lead to more efficiency.

Published in American Journal of Aerospace Engineering (Volume 4, Issue 3)
DOI 10.11648/j.ajae.20170403.11
Page(s) 27-37
Creative Commons

This is an Open Access article, distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium or format, provided the original work is properly cited.

Copyright

Copyright © The Author(s), 2018. Published by Science Publishing Group

Keywords

Natural Convection, Surface Radiation, Conduction, Turbulent Flow and Heat Source

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    Soroush Sadripour, Seyed Amin Ghorashi, Mohammad Estajloo. (2018). Numerical Investigation of a Corrugated Heat Source Cavity: A Full Convection-Conduction-Radiation Coupling. American Journal of Aerospace Engineering, 4(3), 27-37. https://doi.org/10.11648/j.ajae.20170403.11

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    ACS Style

    Soroush Sadripour; Seyed Amin Ghorashi; Mohammad Estajloo. Numerical Investigation of a Corrugated Heat Source Cavity: A Full Convection-Conduction-Radiation Coupling. Am. J. Aerosp. Eng. 2018, 4(3), 27-37. doi: 10.11648/j.ajae.20170403.11

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    AMA Style

    Soroush Sadripour, Seyed Amin Ghorashi, Mohammad Estajloo. Numerical Investigation of a Corrugated Heat Source Cavity: A Full Convection-Conduction-Radiation Coupling. Am J Aerosp Eng. 2018;4(3):27-37. doi: 10.11648/j.ajae.20170403.11

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  • @article{10.11648/j.ajae.20170403.11,
      author = {Soroush Sadripour and Seyed Amin Ghorashi and Mohammad Estajloo},
      title = {Numerical Investigation of a Corrugated Heat Source Cavity: A Full Convection-Conduction-Radiation Coupling},
      journal = {American Journal of Aerospace Engineering},
      volume = {4},
      number = {3},
      pages = {27-37},
      doi = {10.11648/j.ajae.20170403.11},
      url = {https://doi.org/10.11648/j.ajae.20170403.11},
      eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.ajae.20170403.11},
      abstract = {In present study a numerical analysis of complex heat transfer (turbulent natural convection, conduction and surface thermal radiation) in a rectangular enclosure with a heat source has been carried out. The finite volume method based on SIMPLEC algorithm has been utilized. The effects of Rayleigh number in a range from 108 to 1011, internal surface emissivity 0≤ε˂1 on the fluid flow and heat transfer have been extensively explored. Detailed results including temperature fields, flow profiles, and average Nusselt numbers have been presented. In this investigation it has been tried to study the shape of heat source influence on heat transfer and fluid field in the considered domain. According to results in low emissivity values usage of circular obstacles is recommended. Although in high emissivity values using rectangular obstacles lead to more efficiency.},
     year = {2018}
    }
    

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    T1  - Numerical Investigation of a Corrugated Heat Source Cavity: A Full Convection-Conduction-Radiation Coupling
    AU  - Soroush Sadripour
    AU  - Seyed Amin Ghorashi
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    Y1  - 2018/01/03
    PY  - 2018
    N1  - https://doi.org/10.11648/j.ajae.20170403.11
    DO  - 10.11648/j.ajae.20170403.11
    T2  - American Journal of Aerospace Engineering
    JF  - American Journal of Aerospace Engineering
    JO  - American Journal of Aerospace Engineering
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    PB  - Science Publishing Group
    SN  - 2376-4821
    UR  - https://doi.org/10.11648/j.ajae.20170403.11
    AB  - In present study a numerical analysis of complex heat transfer (turbulent natural convection, conduction and surface thermal radiation) in a rectangular enclosure with a heat source has been carried out. The finite volume method based on SIMPLEC algorithm has been utilized. The effects of Rayleigh number in a range from 108 to 1011, internal surface emissivity 0≤ε˂1 on the fluid flow and heat transfer have been extensively explored. Detailed results including temperature fields, flow profiles, and average Nusselt numbers have been presented. In this investigation it has been tried to study the shape of heat source influence on heat transfer and fluid field in the considered domain. According to results in low emissivity values usage of circular obstacles is recommended. Although in high emissivity values using rectangular obstacles lead to more efficiency.
    VL  - 4
    IS  - 3
    ER  - 

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Author Information
  • Department of Mechanical Engineering, University of Kashan, Kashan, Iran

  • Department of Mechanical Engineering, University of Kashan, Kashan, Iran

  • Department of Mechanical Engineering, University of Kashan, Kashan, Iran

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