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High Temperature Material Processes: An International Quarterly of High-Technology Plasma Processes
SJR: 0.137 SNIP: 0.341 CiteScore™: 0.43

ISSN Печать: 1093-3611
ISSN Онлайн: 1940-4360

Выпуски:
Том 23, 2019 Том 22, 2018 Том 21, 2017 Том 20, 2016 Том 19, 2015 Том 18, 2014 Том 17, 2013 Том 16, 2012 Том 15, 2011 Том 14, 2010 Том 13, 2009 Том 12, 2008 Том 11, 2007 Том 10, 2006 Том 9, 2005 Том 8, 2004 Том 7, 2003 Том 6, 2002 Том 5, 2001 Том 4, 2000 Том 3, 1999 Том 2, 1998 Том 1, 1997

High Temperature Material Processes: An International Quarterly of High-Technology Plasma Processes

DOI: 10.1615/HighTempMatProc.v9.i3.40
pages 363-373

MODELLING OF THE HEAT TRANSFER OF ATOMIC OXYGEN RECOMBINATION ON CERAMICS AND SEMICONDUCTORS TARGETS

C. Guyon
Laboratoire de Génie des Procédés Plasmas et Traitement de Surfaces, Universite Pierre & Marie Curie, 11 rue Pierre et Marie Curie, 75231 Paris Cedex, France
S. Cavadias
Laboratoire Genie Precedes Plasmas - ENSCP 11, rue Pierre et Marie Curie - 75005 Paris- France
M. Moscosa
Laboratoire de Genie des Precedes Plasmas et Traitements de Surfaces Universite Pierre et Marie CURIE (Paris VI) ENSCP - 11, roe Pierre et Marie CURIE 75231 PARIS cedex 05 - France
Jacques Amouroux
Laboratoire de Genie des Precedes Plasmas Universite P. et M. Curie, ENSCP 11 rue P. et M. Curie 75005 Paris France

Краткое описание

The goal of this work is to study the heat and mass transfer phenomena at the solid/gas interface for thermal protection system of space vehicles. Catalycity qualified the heat flux due to the oxygen atoms recombination («gamma» coefficient) and their energy accommodation («beta» coefficient) on the surface of the material. So, we propose an approach to modelling and to simulate the recombination of oxygen atoms and the energy transfer to a metallic surface at stagnation point configuration by using a computational fluid dynamics code. The flow is described by a system of conservation (momentum, mass and energy) equations. The necessary boundary conditions were provided by a model for a reactive flow-surface interaction. We have obtained the field velocity, temperature and the fluxes of atomic and molecular oxygen in the reactor under similar conditions to experiments. Assuming surface recombination of oxygen atoms only, the "gamma" coefficient was calculated from the ratios of atomic and molecular fluxes to the surface. The simulation was made on ceramics and semiconductors materials. The comparison between calculated values of "gamma" and experimental ones leads to the determination of the surface recombination rate constants.


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