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Impact of the external energy supply to the shock layer region on the shock wave parameters. / Golyatin, V. Yu; Kuchinskii, V. V.; Sukhomlinov, V. S.

в: Technical Physics, Том 50, № 4, 04.2005, стр. 408-414.

Результаты исследований: Научные публикации в периодических изданияхстатьяРецензирование

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Golyatin, V. Yu ; Kuchinskii, V. V. ; Sukhomlinov, V. S. / Impact of the external energy supply to the shock layer region on the shock wave parameters. в: Technical Physics. 2005 ; Том 50, № 4. стр. 408-414.

BibTeX

@article{277b5314dc63404c9568569805edc5c1,
title = "Impact of the external energy supply to the shock layer region on the shock wave parameters",
abstract = "A system of equations describing supersonic gas flow in the presence of a heat source near the shock front is obtained. Relations between the gas parameters in disturbed and undisturbed regions, which generalize the classical Hugoniot-Rankine relations, are derived. Formulas for calculation of the flow parameters in the presence of an energy supply to the shock layer region are presented. It is demonstrated that there exists a critical intensity of energy supply at which the system of equations of the conservation laws for the gas parameters on both sides of the shock layer possesses no stationary solution.",
author = "Golyatin, {V. Yu} and Kuchinskii, {V. V.} and Sukhomlinov, {V. S.}",
year = "2005",
month = apr,
doi = "10.1134/1.1901777",
language = "English",
volume = "50",
pages = "408--414",
journal = "Technical Physics",
issn = "1063-7842",
publisher = "Pleiades Publishing",
number = "4",

}

RIS

TY - JOUR

T1 - Impact of the external energy supply to the shock layer region on the shock wave parameters

AU - Golyatin, V. Yu

AU - Kuchinskii, V. V.

AU - Sukhomlinov, V. S.

PY - 2005/4

Y1 - 2005/4

N2 - A system of equations describing supersonic gas flow in the presence of a heat source near the shock front is obtained. Relations between the gas parameters in disturbed and undisturbed regions, which generalize the classical Hugoniot-Rankine relations, are derived. Formulas for calculation of the flow parameters in the presence of an energy supply to the shock layer region are presented. It is demonstrated that there exists a critical intensity of energy supply at which the system of equations of the conservation laws for the gas parameters on both sides of the shock layer possesses no stationary solution.

AB - A system of equations describing supersonic gas flow in the presence of a heat source near the shock front is obtained. Relations between the gas parameters in disturbed and undisturbed regions, which generalize the classical Hugoniot-Rankine relations, are derived. Formulas for calculation of the flow parameters in the presence of an energy supply to the shock layer region are presented. It is demonstrated that there exists a critical intensity of energy supply at which the system of equations of the conservation laws for the gas parameters on both sides of the shock layer possesses no stationary solution.

UR - http://www.scopus.com/inward/record.url?scp=17444409303&partnerID=8YFLogxK

U2 - 10.1134/1.1901777

DO - 10.1134/1.1901777

M3 - Article

AN - SCOPUS:17444409303

VL - 50

SP - 408

EP - 414

JO - Technical Physics

JF - Technical Physics

SN - 1063-7842

IS - 4

ER -

ID: 9653000