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Experimental Investigation and Computer Analysis of Sontaneous Condensation in Stationary Nozzle Flow of CO2-Air Mixtures

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Adiabatic Waves in Liquid-Vapor Systems

Summary

The influence of an admixture of air on the onset and the progress of spontaneous condensation of carbon dioxide in a stationary supersonic nozzle flow has been studied for mixtures with CO2-mole fractions ranging from 5 to 75 per cent. For mole fractious of 75 and 50 per cent, the supersaturation of the carbon dioxide at the Wilson point is scarcely influenced by the addition of air. In the range of lower CO2-concentrations, the condensation of carbon dioxide is promoted by the presence of the non-condensing component, as was to be expected from various results reported in the literature.

The thermodynamic state in the Wilson point and the progress of condensation in the flow were calculated with a model of the condensation process based on the classical nucleation model and a formulation of droplet growth proposed by Gyarmathy. It is remarkable that the results of the calculation, obtained with a uniform choice of the free parameters of this condensation model, agree well with the experimental results, both for pure CO2 and for CO2/air-mixtures.

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References

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© 1990 Springer-Verlag Berlin Heidelberg

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Bier, K., Ehrler, F., Niekrawietz, M. (1990). Experimental Investigation and Computer Analysis of Sontaneous Condensation in Stationary Nozzle Flow of CO2-Air Mixtures. In: Meier, G.E.A., Thompson, P.A. (eds) Adiabatic Waves in Liquid-Vapor Systems. International Union of Theoretical and Applied Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-83587-2_11

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  • DOI: https://doi.org/10.1007/978-3-642-83587-2_11

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-83589-6

  • Online ISBN: 978-3-642-83587-2

  • eBook Packages: Springer Book Archive

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