International audienceTo predict the nonequilibrium flows around a hypersonic vehicle entering the Martian atmosphere, the two-temperature collisional-radiative model “CoRaM-MARS” has been developed. The species CO2, CO, C2, CN, N2, NO, O2, C, N, O, Ar, CO+, C+2, CN+, N+2, NO+, O+2, C+, N+, O+, Ar+, and free electrons are taken into account. The model can therefore be used for conditions belonging to wide ranges of temperatures and pressures. The model is vibrationally specific on the ground electronic state of CO2, CO, C2, CN, N2, NO, and O2 and electronically specific for all species, with a total of almost 445 vibrational states and 1139 electronic states, respectively. Due to the high temperatures involved (∼40 000 K), a wide set of ele...
International audienceNonequilibrium infrared emission spectra representative of a Mars atmospheric ...
International audienceThe aim of this paper is to develop a line by line model for CO2 vibrational n...
Calculation of thermodynamic and transport properties of CO2/N2/O2/Ar system (Martian atmosphere) ha...
International audienceTo predict the nonequilibrium flows around a hypersonic vehicle entering the M...
WOS:000346661100049International audienceThree Collisional-Radiative (CR) models are elaborated and ...
WOS:000347162700105International audienceThe two-temperature collisional-radiative model CoRaM-AIR, ...
The hypersonic entry of a body into the upper layers of a planetary atmosphere leads to the formatio...
International audienceThe most relevant way to predict the excited state number density in a nonequi...
This thesis investigates the modelling of radiating shock layers encountered during atmospheric entr...
The mechanism of CO2 dissociation during entry in the Mars atmosphere is experimentally investigated...
A nonlinear time-dependent two-temperature collisional-radiative model for air plasma has been devel...
An electronic state-to-state approach is developed to reproduce numerically the radiative processes ...
A partially electronically specific chemical kinetic model for shock heated CO2-N2 mixtures is imple...
International audienceNonequilibrium infrared emission spectra representative of a Mars atmospheric ...
International audienceThe aim of this paper is to develop a line by line model for CO2 vibrational n...
Calculation of thermodynamic and transport properties of CO2/N2/O2/Ar system (Martian atmosphere) ha...
International audienceTo predict the nonequilibrium flows around a hypersonic vehicle entering the M...
WOS:000346661100049International audienceThree Collisional-Radiative (CR) models are elaborated and ...
WOS:000347162700105International audienceThe two-temperature collisional-radiative model CoRaM-AIR, ...
The hypersonic entry of a body into the upper layers of a planetary atmosphere leads to the formatio...
International audienceThe most relevant way to predict the excited state number density in a nonequi...
This thesis investigates the modelling of radiating shock layers encountered during atmospheric entr...
The mechanism of CO2 dissociation during entry in the Mars atmosphere is experimentally investigated...
A nonlinear time-dependent two-temperature collisional-radiative model for air plasma has been devel...
An electronic state-to-state approach is developed to reproduce numerically the radiative processes ...
A partially electronically specific chemical kinetic model for shock heated CO2-N2 mixtures is imple...
International audienceNonequilibrium infrared emission spectra representative of a Mars atmospheric ...
International audienceThe aim of this paper is to develop a line by line model for CO2 vibrational n...
Calculation of thermodynamic and transport properties of CO2/N2/O2/Ar system (Martian atmosphere) ha...