Finite element modeling of thermal stresses in aerospace structures from polymer composite materials

The conjugate problem of aerodynamics and heat and mass transfer in heat-shielding structures made of ablating polymer composite materials is considered. To determine the heat fluxes in the shock layer, the chemical composition of the atmosphere is taken into account. A mathematical formulation of t...

Full description

Bibliographic Details
Main Authors: Dimitrienko Yuriy, Koryakov Mikhail, Yurin Yuriy, Sborshchikov Sergey, Bogdanov Ilya
Format: Article
Language:English
Published: EDP Sciences 2023-01-01
Series:E3S Web of Conferences
Subjects:
Online Access:https://www.e3s-conferences.org/articles/e3sconf/pdf/2023/13/e3sconf_ersme2023_01033.pdf
_version_ 1797850806306734080
author Dimitrienko Yuriy
Koryakov Mikhail
Yurin Yuriy
Sborshchikov Sergey
Bogdanov Ilya
author_facet Dimitrienko Yuriy
Koryakov Mikhail
Yurin Yuriy
Sborshchikov Sergey
Bogdanov Ilya
author_sort Dimitrienko Yuriy
collection DOAJ
description The conjugate problem of aerodynamics and heat and mass transfer in heat-shielding structures made of ablating polymer composite materials is considered. To determine the heat fluxes in the shock layer, the chemical composition of the atmosphere is taken into account. A mathematical formulation of the joint problem is formulated and an algorithm for numerical solution is proposed. An example of a numerical solution of the problem for the reentry spacecraft Stardust is presented. It is shown that due to the high temperatures of aerodynamic heating of a structure made of a polymer composite material, an intense internal generation of gas appears in the structure of the material, which can lead to the destruction of the material.
first_indexed 2024-04-09T19:07:31Z
format Article
id doaj.art-de22af51470b41d5bc3c1db58ebdec4b
institution Directory Open Access Journal
issn 2267-1242
language English
last_indexed 2024-04-09T19:07:31Z
publishDate 2023-01-01
publisher EDP Sciences
record_format Article
series E3S Web of Conferences
spelling doaj.art-de22af51470b41d5bc3c1db58ebdec4b2023-04-07T08:57:40ZengEDP SciencesE3S Web of Conferences2267-12422023-01-013760103310.1051/e3sconf/202337601033e3sconf_ersme2023_01033Finite element modeling of thermal stresses in aerospace structures from polymer composite materialsDimitrienko Yuriy0Koryakov Mikhail1Yurin Yuriy2Sborshchikov Sergey3Bogdanov Ilya4Bauman Moscow State Technical University 5Bauman Moscow State Technical University 5Bauman Moscow State Technical University 5Bauman Moscow State Technical University 5Bauman Moscow State Technical University 5The conjugate problem of aerodynamics and heat and mass transfer in heat-shielding structures made of ablating polymer composite materials is considered. To determine the heat fluxes in the shock layer, the chemical composition of the atmosphere is taken into account. A mathematical formulation of the joint problem is formulated and an algorithm for numerical solution is proposed. An example of a numerical solution of the problem for the reentry spacecraft Stardust is presented. It is shown that due to the high temperatures of aerodynamic heating of a structure made of a polymer composite material, an intense internal generation of gas appears in the structure of the material, which can lead to the destruction of the material.https://www.e3s-conferences.org/articles/e3sconf/pdf/2023/13/e3sconf_ersme2023_01033.pdfpolymer composite materialfinite elementaerodynamic heatingmathematical formulation
spellingShingle Dimitrienko Yuriy
Koryakov Mikhail
Yurin Yuriy
Sborshchikov Sergey
Bogdanov Ilya
Finite element modeling of thermal stresses in aerospace structures from polymer composite materials
E3S Web of Conferences
polymer composite material
finite element
aerodynamic heating
mathematical formulation
title Finite element modeling of thermal stresses in aerospace structures from polymer composite materials
title_full Finite element modeling of thermal stresses in aerospace structures from polymer composite materials
title_fullStr Finite element modeling of thermal stresses in aerospace structures from polymer composite materials
title_full_unstemmed Finite element modeling of thermal stresses in aerospace structures from polymer composite materials
title_short Finite element modeling of thermal stresses in aerospace structures from polymer composite materials
title_sort finite element modeling of thermal stresses in aerospace structures from polymer composite materials
topic polymer composite material
finite element
aerodynamic heating
mathematical formulation
url https://www.e3s-conferences.org/articles/e3sconf/pdf/2023/13/e3sconf_ersme2023_01033.pdf
work_keys_str_mv AT dimitrienkoyuriy finiteelementmodelingofthermalstressesinaerospacestructuresfrompolymercompositematerials
AT koryakovmikhail finiteelementmodelingofthermalstressesinaerospacestructuresfrompolymercompositematerials
AT yurinyuriy finiteelementmodelingofthermalstressesinaerospacestructuresfrompolymercompositematerials
AT sborshchikovsergey finiteelementmodelingofthermalstressesinaerospacestructuresfrompolymercompositematerials
AT bogdanovilya finiteelementmodelingofthermalstressesinaerospacestructuresfrompolymercompositematerials