Master equation study of three-body recombination of nitrogen and oxygen in non-equilibrium hypersonic flows
Abstract
This work aims to study the energy transfer and recombination processes in N2∑g+3 + NSu4 and O2∑g+3 + OP23 chemical systems when the system is suddenly cooled in a 0-D isothermal reactor thereby inducing strong non-equilibrium. A state-to-state (StS) study of the non-equilibrium phenomenon is crucial for developing accurate and efficient reduced-order models that can accurately capture the thermophysics involved. The gas mixture, consisting primarily of atoms at a high initial temperature of 10 000 K, is suddenly plunged into a low-temperature heat bath to simulate non-equilibrium recombination conditions. The population distribution of microscopic energy levels for each system is determined by solving a system of master equations. The conventional assumption of faster equilibration of rotational mode compared to the vibrational mode holds for N2 + N, while it is not a very strong assumption for O2 + O as the two relaxation time scales are comparable. Effective recombination rate constants for the quasi-steady state (QSS) period are calculated using the population distribution obtained by solving the master equations. It was also observed that the relaxation time constants for heating and cooling are different, with the time constant being lower for the cooling case due to anharmonicity effects in expanding flows. An attempt has also been made to use the insights from the StS analysis to determine an accurate binning strategy for the recombination processes involved in the two chemical systems.
Article Details
Journal Info
The Journal of Chemical Physics
American Institute of Physics
Authors (3)
Aakanksha Notey
Center for Hypersonics and Entry Systems Studies (CHESS), University of Illinois at Urbana-Champaign 1 , Urbana, Illinois 61801,
Sung Min Jo
UCF Center of Excellence in Hypersonics and Space Propulsion (HYPERSPACE) 2 , University of Central Florida, Orlando, Florida 32816,
Marco Panesi
Center for Hypersonics and Entry Systems Studies (CHESS), University of Illinois at Urbana-Champaign 1 , Urbana, Illinois 61801,