International audienceIn this study, the effects of different thermo-chemical models on the macroscopic parameters of the flow behind a strong shock wave have been examined. The effect of the geometric average temperature proposed by Park and the effect of the electronic energy are also presented, and two CVD vibration-dissociation coupling models including those of Park and Kuznetsov are also examined and used for comparison. The Park93 chemical kinetic model with 11 species and 49 elementary reactions was used to describe the non-equilibrium air chemistry. The energy exchange model between translational and vibrational modes is described by the Landau-Teller formula, where the species relaxation time is based on the Millikan-White formula...
Significant contributions were made in a four-year interdisciplinary experimental, numerical and the...
A numerical investigation of thermal non-equilibrium flows requires species specific relaxation rate...
The study considers the solution of a number of problems of supersonic and hypersonic gas dynamics u...
International audienceIn this study, the effects of different thermo-chemical models on the macrosco...
In this paper, we study the phenomena of thermo-chemical imbalance in a reactive mono-dimensional fl...
The high temperatures generated in gases by shock waves give rise to physical and chemical phenomena...
The objective of this work is to predict the optimal speed of an aerospace vehicle by aerothermochem...
The present study aims to assess the performance of chemical rate models for species formation in th...
Abstract. The thermally nonequilibrium gases are those in the absence of equilibrium between transla...
International audienceFour different types of macroscopic models developed for the vibration-chemist...
State-to-state and two-temperature theoretical models for high-temperature strongly nonequilibrium ...
Nonequilibrium thermodynamic state and chemical reactions are common features of hypersonic flows. A...
Steady-state one-dimensional flows of five-component air behind a normal shock wave are considered w...
To study the atmospheric reentry phase of a space vehicle, it is necessary tounderstand correctly th...
The thorough understanding of the formation and the relaxation of the plasma produced in the shock l...
Significant contributions were made in a four-year interdisciplinary experimental, numerical and the...
A numerical investigation of thermal non-equilibrium flows requires species specific relaxation rate...
The study considers the solution of a number of problems of supersonic and hypersonic gas dynamics u...
International audienceIn this study, the effects of different thermo-chemical models on the macrosco...
In this paper, we study the phenomena of thermo-chemical imbalance in a reactive mono-dimensional fl...
The high temperatures generated in gases by shock waves give rise to physical and chemical phenomena...
The objective of this work is to predict the optimal speed of an aerospace vehicle by aerothermochem...
The present study aims to assess the performance of chemical rate models for species formation in th...
Abstract. The thermally nonequilibrium gases are those in the absence of equilibrium between transla...
International audienceFour different types of macroscopic models developed for the vibration-chemist...
State-to-state and two-temperature theoretical models for high-temperature strongly nonequilibrium ...
Nonequilibrium thermodynamic state and chemical reactions are common features of hypersonic flows. A...
Steady-state one-dimensional flows of five-component air behind a normal shock wave are considered w...
To study the atmospheric reentry phase of a space vehicle, it is necessary tounderstand correctly th...
The thorough understanding of the formation and the relaxation of the plasma produced in the shock l...
Significant contributions were made in a four-year interdisciplinary experimental, numerical and the...
A numerical investigation of thermal non-equilibrium flows requires species specific relaxation rate...
The study considers the solution of a number of problems of supersonic and hypersonic gas dynamics u...