Influence of radiative heating on a Martian orbiter
| Autor: | Philippe Rivière, David E. Zeitoun, Anouar Soufiani, Lionel Tessé, Olivier Rouzaud, Tristan Soubrie |
|---|---|
| Přispěvatelé: | Laboratoire d'Énergétique Moléculaire et Macroscopique, Combustion (EM2C), CentraleSupélec-Centre National de la Recherche Scientifique (CNRS)-Université Paris Saclay (COmUE), Institut universitaire des systèmes thermiques industriels (IUSTI), Aix Marseille Université (AMU)-Centre National de la Recherche Scientifique (CNRS), Université Paris Saclay (COmUE)-Centre National de la Recherche Scientifique (CNRS)-CentraleSupélec |
| Jazyk: | angličtina |
| Rok vydání: | 2008 |
| Předmět: |
Convection
Coupled heat transfer Monte Carlo method Aerospace Engineering 01 natural sciences 010305 fluids & plasmas law.invention Orbiter Atmospheric radiative transfer codes Optics law 0103 physical sciences Radiative transfer Parametrization (atmospheric modeling) 010306 general physics Monte Carlo Fluid Flow and Transfer Processes Physics business.industry Mechanical Engineering [SPI.PLASMA]Engineering Sciences [physics]/Plasmas [PHYS.MECA.MSMECA]Physics [physics]/Mechanics [physics]/Materials and structures in mechanics [physics.class-ph] Condensed Matter Physics Computational physics Martian atmosphere 13. Climate action Space and Planetary Science Thermal radiation Entry plasma Heat transfer [PHYS.MECA.THER]Physics [physics]/Mechanics [physics]/Thermics [physics.class-ph] business |
| Zdroj: | Journal of Thermophysics and Heat Transfer Journal of Thermophysics and Heat Transfer, 2008, 22 (1), pp.10-19. ⟨10.2514/1.28259⟩ Journal of Thermophysics and Heat Transfer, American Institute of Aeronautics and Astronautics, 2008, 22 (1), pp.10-19. ⟨10.2514/1.28259⟩ |
| ISSN: | 0887-8722 |
| DOI: | 10.2514/1.28259⟩ |
| Popis: | A computational platform was developed to study radiation of high-temperature gases during atmospheric reentries. This platform includes a 2-D axisymmetrical Navier-Stokes solver and a radiative heat transfer solver based on a Monte Carlo method. In this paper, only gas radiation occurring during entries in the Martian atmosphere is considered. Gas radiative properties are obtained using a statistical narrowband model for CO and CO 2 molecules in high-temperature and low-pressure conditions. Computations on a test case related to the Mars sample return orbiter enabled us to set up a calculation methodology that includes a loose coupling of aerothermodynamics and radiative transfer. Monte Carlo band model calculations are validated against line-by-line calculation and a ray-tracing method. Results show that radiative fluxes on the rear part are important in comparison with convective fluxes. They are mostly due to CO 2 infrared radiation. The effects of radiative transfer on the flow structure and temperature fields in both the front shield and the wake regions are discussed. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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