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Is It Possible to Determine Normal Burning Parameters from the Detonation Theory? / Vasil’ev, A. A.

In: Combustion, Explosion and Shock Waves, Vol. 55, No. 4, 01.07.2019, p. 373-383.

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Vasil’ev AA. Is It Possible to Determine Normal Burning Parameters from the Detonation Theory? Combustion, Explosion and Shock Waves. 2019 Jul 1;55(4):373-383. doi: 10.1134/S0010508219040014

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Vasil’ev, A. A. / Is It Possible to Determine Normal Burning Parameters from the Detonation Theory?. In: Combustion, Explosion and Shock Waves. 2019 ; Vol. 55, No. 4. pp. 373-383.

BibTeX

@article{cd836cabfed947768287016b29718ce3,
title = "Is It Possible to Determine Normal Burning Parameters from the Detonation Theory?",
abstract = "Within the framework of the classical one-dimensional theory of detonation based on conservation laws, the lower branch of the adiabat of energy release of the combustible mixture as a geometric place of the points of the final state of the system admits a solution for combustion waves whose propagation velocity Dfl ranges from zero to the deflagration velocity: 0 ⩽ Dfl ⩽ Ddef. The normal burning wave propagation velocity Su is located in this interval (0 ⩽ Su ⩽ Ddef), but it is traditionally calculated with the use of the thermal theory of combustion rather than detonation theory. Various approaches to choosing the final state point on the lower branch of the energy release adiabat for normal burning are analyzed in the present paper. Estimates are provided both for the degree of correspondence of the predicted and experimental velocities of flame propagation and for the degree of correspondence of the qualitative behavior of these dependences on the basis parameters of the mixture. For most hydrocarbon fuels considered in the study, the best agreement with the experimental data on Su is provided by the formula defining the flame velocity Dfl as the mean geometric value between the diffusion velocity Sdiff and deflagration velocity Ddef.",
keywords = "classical detonation theory, conservation laws, equations of heat transfer and diffusion for combustion, normal burning velocity",
author = "Vasil{\textquoteright}ev, {A. A.}",
year = "2019",
month = jul,
day = "1",
doi = "10.1134/S0010508219040014",
language = "English",
volume = "55",
pages = "373--383",
journal = "Combustion, Explosion and Shock Waves",
issn = "0010-5082",
publisher = "Springer New York",
number = "4",

}

RIS

TY - JOUR

T1 - Is It Possible to Determine Normal Burning Parameters from the Detonation Theory?

AU - Vasil’ev, A. A.

PY - 2019/7/1

Y1 - 2019/7/1

N2 - Within the framework of the classical one-dimensional theory of detonation based on conservation laws, the lower branch of the adiabat of energy release of the combustible mixture as a geometric place of the points of the final state of the system admits a solution for combustion waves whose propagation velocity Dfl ranges from zero to the deflagration velocity: 0 ⩽ Dfl ⩽ Ddef. The normal burning wave propagation velocity Su is located in this interval (0 ⩽ Su ⩽ Ddef), but it is traditionally calculated with the use of the thermal theory of combustion rather than detonation theory. Various approaches to choosing the final state point on the lower branch of the energy release adiabat for normal burning are analyzed in the present paper. Estimates are provided both for the degree of correspondence of the predicted and experimental velocities of flame propagation and for the degree of correspondence of the qualitative behavior of these dependences on the basis parameters of the mixture. For most hydrocarbon fuels considered in the study, the best agreement with the experimental data on Su is provided by the formula defining the flame velocity Dfl as the mean geometric value between the diffusion velocity Sdiff and deflagration velocity Ddef.

AB - Within the framework of the classical one-dimensional theory of detonation based on conservation laws, the lower branch of the adiabat of energy release of the combustible mixture as a geometric place of the points of the final state of the system admits a solution for combustion waves whose propagation velocity Dfl ranges from zero to the deflagration velocity: 0 ⩽ Dfl ⩽ Ddef. The normal burning wave propagation velocity Su is located in this interval (0 ⩽ Su ⩽ Ddef), but it is traditionally calculated with the use of the thermal theory of combustion rather than detonation theory. Various approaches to choosing the final state point on the lower branch of the energy release adiabat for normal burning are analyzed in the present paper. Estimates are provided both for the degree of correspondence of the predicted and experimental velocities of flame propagation and for the degree of correspondence of the qualitative behavior of these dependences on the basis parameters of the mixture. For most hydrocarbon fuels considered in the study, the best agreement with the experimental data on Su is provided by the formula defining the flame velocity Dfl as the mean geometric value between the diffusion velocity Sdiff and deflagration velocity Ddef.

KW - classical detonation theory

KW - conservation laws

KW - equations of heat transfer and diffusion for combustion

KW - normal burning velocity

UR - http://www.scopus.com/inward/record.url?scp=85071430491&partnerID=8YFLogxK

U2 - 10.1134/S0010508219040014

DO - 10.1134/S0010508219040014

M3 - Article

AN - SCOPUS:85071430491

VL - 55

SP - 373

EP - 383

JO - Combustion, Explosion and Shock Waves

JF - Combustion, Explosion and Shock Waves

SN - 0010-5082

IS - 4

ER -

ID: 21472771