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State-to-state kinetic modeling of dissociating and radiating hypersonic flows. / Josyula, Eswar; Burt, Jonathan M.; Kustova, Elena; Mekhonoshina, Mariia; Vedula, Prakash.

53rd AIAA Aerospace Sciences Meeting. The American Institute of Aeronautics and Astronautics, 2015. AIAA 2015-0475 (53rd AIAA Aerospace Sciences Meeting).

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Harvard

Josyula, E, Burt, JM, Kustova, E, Mekhonoshina, M & Vedula, P 2015, State-to-state kinetic modeling of dissociating and radiating hypersonic flows. in 53rd AIAA Aerospace Sciences Meeting., AIAA 2015-0475, 53rd AIAA Aerospace Sciences Meeting, The American Institute of Aeronautics and Astronautics, 53rd AIAA Aerospace Sciences Meeting, 2015, Kissimmee, United States, 5/01/15. https://doi.org/10.2514/6.2015-0475, https://doi.org/10.2514/6.2015-0475

APA

Josyula, E., Burt, J. M., Kustova, E., Mekhonoshina, M., & Vedula, P. (2015). State-to-state kinetic modeling of dissociating and radiating hypersonic flows. In 53rd AIAA Aerospace Sciences Meeting [AIAA 2015-0475] (53rd AIAA Aerospace Sciences Meeting). The American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0475, https://doi.org/10.2514/6.2015-0475

Vancouver

Josyula E, Burt JM, Kustova E, Mekhonoshina M, Vedula P. State-to-state kinetic modeling of dissociating and radiating hypersonic flows. In 53rd AIAA Aerospace Sciences Meeting. The American Institute of Aeronautics and Astronautics. 2015. AIAA 2015-0475. (53rd AIAA Aerospace Sciences Meeting). https://doi.org/10.2514/6.2015-0475, https://doi.org/10.2514/6.2015-0475

Author

Josyula, Eswar ; Burt, Jonathan M. ; Kustova, Elena ; Mekhonoshina, Mariia ; Vedula, Prakash. / State-to-state kinetic modeling of dissociating and radiating hypersonic flows. 53rd AIAA Aerospace Sciences Meeting. The American Institute of Aeronautics and Astronautics, 2015. (53rd AIAA Aerospace Sciences Meeting).

BibTeX

@inproceedings{63b895277d8740449835a30adbe94522,
title = "State-to-state kinetic modeling of dissociating and radiating hypersonic flows",
abstract = "Studies based on the numerical simulations are presented for hypersonic blunt body and normal shock flows involving thermo-chemical nonequilibrium and radiation phenomena. The internal energy relaxation processes of vibrational energy transfer, dissociation, and radiation are treated using a state-to-state kinetics approach. A set of dissociation studies are conducted for a nitrogen gas flow past a blunt body, and coupled physico-chemical and radiative processes are investigated for flow behind a shock wave. The surface heat flux on the body is determined through a rigorous kinetic theory algorithm for the calculation of statetostate transport properties, such that diffusion velocities and heat flux are accounted for in the dissipative processes in the flow. Contributions to heat flux are considered for heat conduction, thermal diffusion, mass diffusion, and diffusion of vibrational energy. For the Mach 19.83 conditions, thermal diffusion is the dominant contributor to surface heat flux, and vibrational energy diffusion is also found to be a significant contributor. Radiation modeling is performed using a state to state approach which incorporates procedures for vibrational-translational and vibrational-electronic energy exchange as well as state-specific dissociation. It is found that radiative emission is very sensitive to dissociation product concentrations, and the evolution of the macroscopic gas parameters is essentially governed by the behavior of most populated species in their ground electronic states. The radiation intensity is mainly governed by spontaneous emission processes, which in turn result in significant depletion in the population of N2 in the excited B3П state.",
author = "Eswar Josyula and Burt, {Jonathan M.} and Elena Kustova and Mariia Mekhonoshina and Prakash Vedula",
note = "Publisher Copyright: {\textcopyright} 2015, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. Copyright: Copyright 2016 Elsevier B.V., All rights reserved.; 53rd AIAA Aerospace Sciences Meeting, 2015 ; Conference date: 05-01-2015 Through 09-01-2015",
year = "2015",
doi = "10.2514/6.2015-0475",
language = "English",
isbn = "9781624103438",
series = "53rd AIAA Aerospace Sciences Meeting",
publisher = "The American Institute of Aeronautics and Astronautics",
booktitle = "53rd AIAA Aerospace Sciences Meeting",
address = "United States",

}

RIS

TY - GEN

T1 - State-to-state kinetic modeling of dissociating and radiating hypersonic flows

AU - Josyula, Eswar

AU - Burt, Jonathan M.

AU - Kustova, Elena

AU - Mekhonoshina, Mariia

AU - Vedula, Prakash

N1 - Publisher Copyright: © 2015, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. Copyright: Copyright 2016 Elsevier B.V., All rights reserved.

PY - 2015

Y1 - 2015

N2 - Studies based on the numerical simulations are presented for hypersonic blunt body and normal shock flows involving thermo-chemical nonequilibrium and radiation phenomena. The internal energy relaxation processes of vibrational energy transfer, dissociation, and radiation are treated using a state-to-state kinetics approach. A set of dissociation studies are conducted for a nitrogen gas flow past a blunt body, and coupled physico-chemical and radiative processes are investigated for flow behind a shock wave. The surface heat flux on the body is determined through a rigorous kinetic theory algorithm for the calculation of statetostate transport properties, such that diffusion velocities and heat flux are accounted for in the dissipative processes in the flow. Contributions to heat flux are considered for heat conduction, thermal diffusion, mass diffusion, and diffusion of vibrational energy. For the Mach 19.83 conditions, thermal diffusion is the dominant contributor to surface heat flux, and vibrational energy diffusion is also found to be a significant contributor. Radiation modeling is performed using a state to state approach which incorporates procedures for vibrational-translational and vibrational-electronic energy exchange as well as state-specific dissociation. It is found that radiative emission is very sensitive to dissociation product concentrations, and the evolution of the macroscopic gas parameters is essentially governed by the behavior of most populated species in their ground electronic states. The radiation intensity is mainly governed by spontaneous emission processes, which in turn result in significant depletion in the population of N2 in the excited B3П state.

AB - Studies based on the numerical simulations are presented for hypersonic blunt body and normal shock flows involving thermo-chemical nonequilibrium and radiation phenomena. The internal energy relaxation processes of vibrational energy transfer, dissociation, and radiation are treated using a state-to-state kinetics approach. A set of dissociation studies are conducted for a nitrogen gas flow past a blunt body, and coupled physico-chemical and radiative processes are investigated for flow behind a shock wave. The surface heat flux on the body is determined through a rigorous kinetic theory algorithm for the calculation of statetostate transport properties, such that diffusion velocities and heat flux are accounted for in the dissipative processes in the flow. Contributions to heat flux are considered for heat conduction, thermal diffusion, mass diffusion, and diffusion of vibrational energy. For the Mach 19.83 conditions, thermal diffusion is the dominant contributor to surface heat flux, and vibrational energy diffusion is also found to be a significant contributor. Radiation modeling is performed using a state to state approach which incorporates procedures for vibrational-translational and vibrational-electronic energy exchange as well as state-specific dissociation. It is found that radiative emission is very sensitive to dissociation product concentrations, and the evolution of the macroscopic gas parameters is essentially governed by the behavior of most populated species in their ground electronic states. The radiation intensity is mainly governed by spontaneous emission processes, which in turn result in significant depletion in the population of N2 in the excited B3П state.

UR - http://www.scopus.com/inward/record.url?scp=84980332332&partnerID=8YFLogxK

U2 - 10.2514/6.2015-0475

DO - 10.2514/6.2015-0475

M3 - Conference contribution

SN - 9781624103438

T3 - 53rd AIAA Aerospace Sciences Meeting

BT - 53rd AIAA Aerospace Sciences Meeting

PB - The American Institute of Aeronautics and Astronautics

T2 - 53rd AIAA Aerospace Sciences Meeting, 2015

Y2 - 5 January 2015 through 9 January 2015

ER -

ID: 3926406