Implementation of Surface Radiation and Fluid-Structure Thermal Coupling in Atmospheric Reentry

During atmospheric reentry, radiative heating is one of the most important component of the total heat flux. In this paper, we investigate how the thermal radiation coming from the postshock region interacts with the spacecraft structure. A model that takes into account the radiation reflected by th...

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Main Authors: Ojas Joshi, Pénélope Leyland
Format: Article
Language:English
Published: Wiley 2012-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2012/402653
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author Ojas Joshi
Pénélope Leyland
author_facet Ojas Joshi
Pénélope Leyland
author_sort Ojas Joshi
collection DOAJ
description During atmospheric reentry, radiative heating is one of the most important component of the total heat flux. In this paper, we investigate how the thermal radiation coming from the postshock region interacts with the spacecraft structure. A model that takes into account the radiation reflected by the surface is developed and implemented in a solid solver. A partitioned algorithm performs the coupling between the fluid and the solid thermal fields. Numerical simulation of a hollow cone head and a deployed flap region shows the effects of the radiative cooling and the significance of the surface radiation.
format Article
id doaj-art-7e3e2ad184ca4c169eb81894c34e0c70
institution Kabale University
issn 1687-5966
1687-5974
language English
publishDate 2012-01-01
publisher Wiley
record_format Article
series International Journal of Aerospace Engineering
spelling doaj-art-7e3e2ad184ca4c169eb81894c34e0c702025-02-03T05:57:34ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742012-01-01201210.1155/2012/402653402653Implementation of Surface Radiation and Fluid-Structure Thermal Coupling in Atmospheric ReentryOjas Joshi0Pénélope Leyland1Ecole Polytechnique Fédérale de Lausanne, Interdisciplinary Aerodynamics Group, Station 9, 1015 Lausanne, SwitzerlandEcole Polytechnique Fédérale de Lausanne, Interdisciplinary Aerodynamics Group, Station 9, 1015 Lausanne, SwitzerlandDuring atmospheric reentry, radiative heating is one of the most important component of the total heat flux. In this paper, we investigate how the thermal radiation coming from the postshock region interacts with the spacecraft structure. A model that takes into account the radiation reflected by the surface is developed and implemented in a solid solver. A partitioned algorithm performs the coupling between the fluid and the solid thermal fields. Numerical simulation of a hollow cone head and a deployed flap region shows the effects of the radiative cooling and the significance of the surface radiation.http://dx.doi.org/10.1155/2012/402653
spellingShingle Ojas Joshi
Pénélope Leyland
Implementation of Surface Radiation and Fluid-Structure Thermal Coupling in Atmospheric Reentry
International Journal of Aerospace Engineering
title Implementation of Surface Radiation and Fluid-Structure Thermal Coupling in Atmospheric Reentry
title_full Implementation of Surface Radiation and Fluid-Structure Thermal Coupling in Atmospheric Reentry
title_fullStr Implementation of Surface Radiation and Fluid-Structure Thermal Coupling in Atmospheric Reentry
title_full_unstemmed Implementation of Surface Radiation and Fluid-Structure Thermal Coupling in Atmospheric Reentry
title_short Implementation of Surface Radiation and Fluid-Structure Thermal Coupling in Atmospheric Reentry
title_sort implementation of surface radiation and fluid structure thermal coupling in atmospheric reentry
url http://dx.doi.org/10.1155/2012/402653
work_keys_str_mv AT ojasjoshi implementationofsurfaceradiationandfluidstructurethermalcouplinginatmosphericreentry
AT penelopeleyland implementationofsurfaceradiationandfluidstructurethermalcouplinginatmosphericreentry