Standard

State-to-state and multi-temperature models of transport properties in reacting gas flows. / Kustova, EV; Nagnibeda, EA.

PROCEEDINGS OF THE THIRD EUROPEAN SYMPOSIUM ON AEROTHERMODYNAMICS FOR SPACE VEHICLES. ed. / RA Harris. ESA Publication Division, 1999. p. 269-274 (ESA SPECIAL PUBLICATIONS; Vol. 420).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Research › peer-review

Harvard

Kustova, EV & Nagnibeda, EA 1999, State-to-state and multi-temperature models of transport properties in reacting gas flows. in RA Harris (ed.), PROCEEDINGS OF THE THIRD EUROPEAN SYMPOSIUM ON AEROTHERMODYNAMICS FOR SPACE VEHICLES. ESA SPECIAL PUBLICATIONS, vol. 420, ESA Publication Division, pp. 269-274, 3rd European Symposium on Aerothermodynamics for Space Vehicles, NOORDWIJK, Netherlands, 24/11/98.

APA

Kustova, EV., & Nagnibeda, EA. (1999). State-to-state and multi-temperature models of transport properties in reacting gas flows. In RA. Harris (Ed.), PROCEEDINGS OF THE THIRD EUROPEAN SYMPOSIUM ON AEROTHERMODYNAMICS FOR SPACE VEHICLES (pp. 269-274). (ESA SPECIAL PUBLICATIONS; Vol. 420). ESA Publication Division.

Vancouver

Kustova EV, Nagnibeda EA. State-to-state and multi-temperature models of transport properties in reacting gas flows. In Harris RA, editor, PROCEEDINGS OF THE THIRD EUROPEAN SYMPOSIUM ON AEROTHERMODYNAMICS FOR SPACE VEHICLES. ESA Publication Division. 1999. p. 269-274. (ESA SPECIAL PUBLICATIONS).

Author

Kustova, EV ; Nagnibeda, EA. / State-to-state and multi-temperature models of transport properties in reacting gas flows. PROCEEDINGS OF THE THIRD EUROPEAN SYMPOSIUM ON AEROTHERMODYNAMICS FOR SPACE VEHICLES. editor / RA Harris. ESA Publication Division, 1999. pp. 269-274 (ESA SPECIAL PUBLICATIONS).

BibTeX

@inproceedings{9bb4553ddd914444916f3b391291ad9c,
title = "State-to-state and multi-temperature models of transport properties in reacting gas flows",
abstract = "The aim of the present paper is the development of efficient models of nonequilibrium transport properties to be used in the computational Navier-Stokes codes for the calculation of the flow parameters in a shock heated gas around reentering vehicles. The multi-level transport kinetic theory is applied for the conditions behind plane shock waves, the heat transfer and diffusion are investigated. Binary mixtures of atoms and molecules with dissociation, recombination and various vibrational energy exchanges are considered. The effect of the different interaction potentials on the transport properties is evaluated. The results are compared with the ones obtained in the two-temperature and one-temperature approximation.",
keywords = "nonequilibrium flow, transport properties, POLYATOMIC GASES, NONEQUILIBRIUM, DISSOCIATION, MIXTURE",
author = "EV Kustova and EA Nagnibeda",
year = "1999",
language = "Английский",
isbn = "92-9092-704-6",
series = "ESA SPECIAL PUBLICATIONS",
publisher = "ESA Publication Division",
pages = "269--274",
editor = "RA Harris",
booktitle = "PROCEEDINGS OF THE THIRD EUROPEAN SYMPOSIUM ON AEROTHERMODYNAMICS FOR SPACE VEHICLES",
address = "Франция",
note = "null ; Conference date: 24-11-1998 Through 26-11-1998",

}

RIS

TY - GEN

T1 - State-to-state and multi-temperature models of transport properties in reacting gas flows

AU - Kustova, EV

AU - Nagnibeda, EA

PY - 1999

Y1 - 1999

N2 - The aim of the present paper is the development of efficient models of nonequilibrium transport properties to be used in the computational Navier-Stokes codes for the calculation of the flow parameters in a shock heated gas around reentering vehicles. The multi-level transport kinetic theory is applied for the conditions behind plane shock waves, the heat transfer and diffusion are investigated. Binary mixtures of atoms and molecules with dissociation, recombination and various vibrational energy exchanges are considered. The effect of the different interaction potentials on the transport properties is evaluated. The results are compared with the ones obtained in the two-temperature and one-temperature approximation.

AB - The aim of the present paper is the development of efficient models of nonequilibrium transport properties to be used in the computational Navier-Stokes codes for the calculation of the flow parameters in a shock heated gas around reentering vehicles. The multi-level transport kinetic theory is applied for the conditions behind plane shock waves, the heat transfer and diffusion are investigated. Binary mixtures of atoms and molecules with dissociation, recombination and various vibrational energy exchanges are considered. The effect of the different interaction potentials on the transport properties is evaluated. The results are compared with the ones obtained in the two-temperature and one-temperature approximation.

KW - nonequilibrium flow

KW - transport properties

KW - POLYATOMIC GASES

KW - NONEQUILIBRIUM

KW - DISSOCIATION

KW - MIXTURE

M3 - статья в сборнике материалов конференции

SN - 92-9092-704-6

T3 - ESA SPECIAL PUBLICATIONS

SP - 269

EP - 274

BT - PROCEEDINGS OF THE THIRD EUROPEAN SYMPOSIUM ON AEROTHERMODYNAMICS FOR SPACE VEHICLES

A2 - Harris, RA

PB - ESA Publication Division

Y2 - 24 November 1998 through 26 November 1998

ER -

ID: 85898095