46th AIAA Thermophysics Conference 2016
DOI: 10.2514/6.2016-3842
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Finite-rate oxidation model for carbon surfaces from molecular beam experiments

Abstract: An oxidation model for carbon surfaces is developed where the gas-surface reaction mechanisms and corresponding rate parameters are based solely on observations from recent molecular beam experiments. In the experiments, a high energy beam of oxygen (93% atoms and 7% molecules) was directed at a high-temperature carbon surface. The measurements revealed that CO was the dominant reaction product and that its formation required a high surface coverage of oxygen atoms. As the carbon sample temperature was increas… Show more

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Cited by 6 publications
(6 citation statements)
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References 43 publications
(41 reference statements)
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“…5a and 7a for FiberForm and vitreous carbon respectively, for both the increasing and the decreasing temperature surveys. The TD-prompt flux increases markedly beyond 1200 K for vitreous carbon which may be ascribed to surface-adsorbed O desorbing promptly as the surface temperature is increased [5,27,28]. A similar trend is observed for FiberForm, where the TD-prompt flux dominates beyond 1300 K. However, the rate of TD-prompt flux increase for vitreous carbon is approximately 2.8 times faster than for FiberForm.…”
Section: Inelastic and Reactive Scattering Of O And O2 From Fiberformsupporting
confidence: 55%
See 1 more Smart Citation
“…5a and 7a for FiberForm and vitreous carbon respectively, for both the increasing and the decreasing temperature surveys. The TD-prompt flux increases markedly beyond 1200 K for vitreous carbon which may be ascribed to surface-adsorbed O desorbing promptly as the surface temperature is increased [5,27,28]. A similar trend is observed for FiberForm, where the TD-prompt flux dominates beyond 1300 K. However, the rate of TD-prompt flux increase for vitreous carbon is approximately 2.8 times faster than for FiberForm.…”
Section: Inelastic and Reactive Scattering Of O And O2 From Fiberformsupporting
confidence: 55%
“…Ablative heat shields are currently overdesigned as a result of large uncertainties [1,4] in the understanding of the oxidation mechanisms. A better understanding of the oxidation process would enable improved carbon-oxygen kinetic rate models for computational fluid dynamics (CFD) [5][6][7] and direct simulation Monte Carlo (DSMC) simulations of heat shield behavior during hypersonic flight [8,9]. The oxidation of a porous carbon network (FiberForm) has been studied in flow-tube experiments where the reactive gas was O2 [10][11][12].…”
Section: Introductionmentioning
confidence: 99%
“…The TD-slow signal decreases as the surface temperature increases, with the TD-slow flux accounting for ~8% of the total flux at 1123 K and ~5% at 1823 K. The flux components of O are shown in Figures 5a and 7a for FiberForm and vitreous carbon respectively, for both the increasing and the decreasing temperature sweeps. The TD-prompt flux increases markedly beyond 1200 K for vitreous carbon, which may be ascribed to surface-adsorbed O desorbing promptly as the surface temperature is increased [5,27,28]. A similar trend is observed for FiberForm, where the TD-prompt flux dominates beyond 1300 K. However, the rate of TDprompt flux increase for vitreous carbon is approximately 2.8 times faster than for FiberForm.…”
Section: Inelastic Andsupporting
confidence: 52%
“…Ablative heat shields are currently overdesigned as a result of large uncertainties in the understanding of the oxidation mechanisms [1,4]. A better understanding of the oxidation process would enable improved carbon-oxygen kinetic rate models for computational fluid dynamics (CFD) [5][6][7] and direct simulation Monte Carlo (DSMC) simulations of heat shield behavior during hypersonic flight [8,9]. The oxidation of a porous carbon network (FiberForm) has been studied in flow-tube experiments where the reactive gas was O2 [10][11][12].…”
Section: Introductionmentioning
confidence: 99%
“…Ablative heat shields are currently overdesigned as a result of large uncertainties in the understanding of the oxidation mechanisms [1,4]. A better understanding of the oxidation process would enable improved carbon-oxygen kinetic rate models for computational fluid dynamics (CFD) [5][6][7] and direct simulation Monte Carlo (DSMC) simulations of heat shield behavior during hypersonic flight [8,9]. The oxidation of a porous carbon network (FiberForm) has been studied in flow-tube experiments where the reactive gas was O2 [10][11][12].…”
Section: Introductionmentioning
confidence: 99%