International audienceNonequilibrium infrared emission spectra representative of a Mars atmospheric entry mission are modeled using RADIS, a spectral code for CO and CO 2 based on the HITEMP-2010 and CDSD-4000 databases. The modeled experimental data for the free-flow and the forebody radiation were obtained in the JAXA expansion tube facility. In the expanding flow, good agreement with the experimental data can be obtained using a slightly nonequilibrium distribution and a homogeneous flow. The model suggests that all three CO 2 vibration modes share a same vibrational temperature slightly higher than the gas temperature. In the shock layer, the forebody radiation includes both CO 2 and CO emission features. It can be correctly predicted b...
When an object is entering the atmosphere of Mars at hypersonic speeds, a detached shock layer is fo...
International audienceAn open-source nonequilibrium emission and absorption infrared line-by-line co...
International audienceTo predict the nonequilibrium flows around a hypersonic vehicle entering the M...
International audienceNonequilibrium infrared emission spectra representative of a Mars atmospheric ...
A model for simulating nonequilibrium radiation from Mars entry shock layers is presented. A new che...
Predicting and managing heat transfer during planetary entry is a critical engineering challenge for...
CO concentration and gas temperature distribution are diagnosed behind a strong shock wave simulatin...
This paper presents simulations of the radiative heat flux imparted on the after-body of vehicles en...
Thermochemical relaxation behind a normal shock in Mars and Titan gas mixtures is simulated using a ...
A computational platform was developed to study radiation of high-temperature gases during atmospher...
This thesis investigates the modelling of radiating shock layers encountered during atmospheric entr...
This paper reports on the measurement of radiative heating for shock heated flows which simulate con...
This paper represents a summary of results to date of an on-going effort at NASA Ames Research Cente...
International audienceThe aim of this paper is to develop a line by line model for CO2 vibrational n...
This work represents ongoing efforts to study high-enthalpy carbon dioxide flows in anticipation of ...
When an object is entering the atmosphere of Mars at hypersonic speeds, a detached shock layer is fo...
International audienceAn open-source nonequilibrium emission and absorption infrared line-by-line co...
International audienceTo predict the nonequilibrium flows around a hypersonic vehicle entering the M...
International audienceNonequilibrium infrared emission spectra representative of a Mars atmospheric ...
A model for simulating nonequilibrium radiation from Mars entry shock layers is presented. A new che...
Predicting and managing heat transfer during planetary entry is a critical engineering challenge for...
CO concentration and gas temperature distribution are diagnosed behind a strong shock wave simulatin...
This paper presents simulations of the radiative heat flux imparted on the after-body of vehicles en...
Thermochemical relaxation behind a normal shock in Mars and Titan gas mixtures is simulated using a ...
A computational platform was developed to study radiation of high-temperature gases during atmospher...
This thesis investigates the modelling of radiating shock layers encountered during atmospheric entr...
This paper reports on the measurement of radiative heating for shock heated flows which simulate con...
This paper represents a summary of results to date of an on-going effort at NASA Ames Research Cente...
International audienceThe aim of this paper is to develop a line by line model for CO2 vibrational n...
This work represents ongoing efforts to study high-enthalpy carbon dioxide flows in anticipation of ...
When an object is entering the atmosphere of Mars at hypersonic speeds, a detached shock layer is fo...
International audienceAn open-source nonequilibrium emission and absorption infrared line-by-line co...
International audienceTo predict the nonequilibrium flows around a hypersonic vehicle entering the M...