CO2 IR radiation modelling with a multi-temperature approach in flows under vibrational nonequilibrium. (December 2019)

• Record Type: Journal Article
• Authors: Binauld, Quentin; Rivière, Philippe; Lamet, Jean-Michel; Tessé, Lionel; Soufiani, Anouar
• Is Part Of: Journal of quantitative spectroscopy & radiative transfer. Volume 239(2019)
• Publication Date: 2019-12
• Subjects: CO2 radiation -- Vibrational nonequilibrium -- Multi-temperature model -- Expanding jets; Spectrum analysis -- Periodicals; Radiation -- Periodicals; Analyse spectrale -- Périodiques; Rayonnement -- Périodiques; Radiation; Spectrum analysis; Periodicals; 543.0858
• DOI: 10.1016/j.jqsrt.2019.106652
• Languages: English
• ISSNs: 0022-4073

Abstract

Highlights: A consistent model for CO2 radiation under nonequilibrium conditions is developed. Vibrational radiation source terms are derived from partial absorption and emission coefficients. Vibrational temperature fields are obtained from Lagrangian post-processing of equilibrium calculations. The model is applied to a nozzle expanding flow and to a high altitude rocket plume. Emitted radiation is significantly increased due to the partial freeze of vibrational excitation. Abstract: The aim of this paper is to develop a line by line model for CO2 vibrational nonequilibrium radiation and to investigate nonequilibrium effects in the case of some applications involving high temperature expanding flows. A vibrational specific collisional relaxation model is developed and is incorporated in a multi-temperature thermodynamic description of the gas mixture, in order to compute vibrational level populations along the flow. The HITEMP-2010 spectroscopic database is employed with a model for level energy splitting to provide line by line absorption and emission total and per-vibrational mode specific spectra. The specific spectra allow us to derive the radiative source terms to be used in the multi-temperature model if a coupled approach is required. The model is applied first to a simple conical nozzle flow and then to the plume of a high altitude solid propellant rocket engine. It is shown that, for the considered applications, the partial freeze of vibrational excitation in the expanding flow increases significantly the radiative intensity escaping from the mixture.