Heat Transfer in Pure Oxygen Flow around a Probe in Comete Facility

Details Heat Transfer in Pure Oxygen Flow around a Probe in Comete Facility Heat Transfer in Pure Oxygen Flow around a Probe in Comete Facility

Feb 2005

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2005esasp.563..109p&link_type=abstract

Proceedings of the Fifth European Symposium on Aerothermodynamics for Space Vehicles (ESA SP-563). 8-11 November 2004, Cologne,

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We present a study of a reactive subsonic flow of pure oxygen over a probe as well as our approach of catalycity from both a chemical and physical point of view. The CFD modelling is developed for a pure oxygen plasma, with physicochemical parameters calculated by Wilke's law for mixtures. In a first step, we included neither deviations from chemical equilibrium nor the reactivity of the interface and solved the full set of Navier-Stokes equations into the whole domain. At the same time, we are studying catalycity from a chemical point of view by performing ab initio calculations on the first elementary step in wall recombination: atomic oxygen adsorption on a copper surface. Key words: Adsorption; Catalycity; Subsonic flow; Ab initio; Oxygen.

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