Standard

On the transient regime in nonstationary supersonic flow past a body. / Bogatko, V. I.; Kolton, G. A.

в: Fluid Dynamics, Том 32, № 1, 01.01.1997, стр. 92-102.

Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование

Harvard

Bogatko, VI & Kolton, GA 1997, 'On the transient regime in nonstationary supersonic flow past a body', Fluid Dynamics, Том. 32, № 1, стр. 92-102. https://doi.org/10.1007/BF02697942

APA

Bogatko, V. I., & Kolton, G. A. (1997). On the transient regime in nonstationary supersonic flow past a body. Fluid Dynamics, 32(1), 92-102. https://doi.org/10.1007/BF02697942

Vancouver

Bogatko VI, Kolton GA. On the transient regime in nonstationary supersonic flow past a body. Fluid Dynamics. 1997 Янв. 1;32(1):92-102. https://doi.org/10.1007/BF02697942

Author

Bogatko, V. I. ; Kolton, G. A. / On the transient regime in nonstationary supersonic flow past a body. в: Fluid Dynamics. 1997 ; Том 32, № 1. стр. 92-102.

BibTeX

@article{d8b7661f88eb415884a42c879652c9fe,
title = "On the transient regime in nonstationary supersonic flow past a body",
abstract = "The transient regime in gas flow past a stepwise accelerated body is analyzed by the method of singular perturbations at small Froude numbers. A marked effect of the initial conditions on the shock layer gas flow is demonstrated. The problem of flow past a wedge is solved in quadratures.",
author = "Bogatko, {V. I.} and Kolton, {G. A.}",
year = "1997",
month = jan,
day = "1",
doi = "10.1007/BF02697942",
language = "English",
volume = "32",
pages = "92--102",
journal = "Fluid Dynamics",
issn = "0015-4628",
publisher = "Springer Nature",
number = "1",

}

RIS

TY - JOUR

T1 - On the transient regime in nonstationary supersonic flow past a body

AU - Bogatko, V. I.

AU - Kolton, G. A.

PY - 1997/1/1

Y1 - 1997/1/1

N2 - The transient regime in gas flow past a stepwise accelerated body is analyzed by the method of singular perturbations at small Froude numbers. A marked effect of the initial conditions on the shock layer gas flow is demonstrated. The problem of flow past a wedge is solved in quadratures.

AB - The transient regime in gas flow past a stepwise accelerated body is analyzed by the method of singular perturbations at small Froude numbers. A marked effect of the initial conditions on the shock layer gas flow is demonstrated. The problem of flow past a wedge is solved in quadratures.

UR - http://www.scopus.com/inward/record.url?scp=27144462137&partnerID=8YFLogxK

U2 - 10.1007/BF02697942

DO - 10.1007/BF02697942

M3 - Article

AN - SCOPUS:27144462137

VL - 32

SP - 92

EP - 102

JO - Fluid Dynamics

JF - Fluid Dynamics

SN - 0015-4628

IS - 1

ER -

ID: 48961585