Standard

The definition of the gas flow parameters in the shock layer near a thin variable form wing moving with a high variable velocity. / Bogatko, V. I.; Kolton, G. A.; Potekhina, E. A.

в: Vestnik Sankt-Peterburgskogo Universiteta. Ser 1. Matematika Mekhanika Astronomiya, № 2, 01.01.2002, стр. 61-66.

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

Harvard

Bogatko, VI, Kolton, GA & Potekhina, EA 2002, 'The definition of the gas flow parameters in the shock layer near a thin variable form wing moving with a high variable velocity', Vestnik Sankt-Peterburgskogo Universiteta. Ser 1. Matematika Mekhanika Astronomiya, № 2, стр. 61-66.

APA

Bogatko, V. I., Kolton, G. A., & Potekhina, E. A. (2002). The definition of the gas flow parameters in the shock layer near a thin variable form wing moving with a high variable velocity. Vestnik Sankt-Peterburgskogo Universiteta. Ser 1. Matematika Mekhanika Astronomiya, (2), 61-66.

Vancouver

Bogatko VI, Kolton GA, Potekhina EA. The definition of the gas flow parameters in the shock layer near a thin variable form wing moving with a high variable velocity. Vestnik Sankt-Peterburgskogo Universiteta. Ser 1. Matematika Mekhanika Astronomiya. 2002 Янв. 1;(2):61-66.

Author

Bogatko, V. I. ; Kolton, G. A. ; Potekhina, E. A. / The definition of the gas flow parameters in the shock layer near a thin variable form wing moving with a high variable velocity. в: Vestnik Sankt-Peterburgskogo Universiteta. Ser 1. Matematika Mekhanika Astronomiya. 2002 ; № 2. стр. 61-66.

BibTeX

@article{1f81657e8fe54a8ca93d34cce3949567,
title = "The definition of the gas flow parameters in the shock layer near a thin variable form wing moving with a high variable velocity",
abstract = "In thin shock layer method is applied to the problem under consideration. A vector of the wing velocity depends on the time. The head shock wave is considered to be joined to the surface of the body at least in an one point. The solution was written for the case when the vertical acceleration component is small.",
author = "Bogatko, {V. I.} and Kolton, {G. A.} and Potekhina, {E. A.}",
year = "2002",
month = jan,
day = "1",
language = "русский",
pages = "61--66",
journal = "ВЕСТНИК САНКТ-ПЕТЕРБУРГСКОГО УНИВЕРСИТЕТА. МАТЕМАТИКА. МЕХАНИКА. АСТРОНОМИЯ",
issn = "1025-3106",
publisher = "Издательство Санкт-Петербургского университета",
number = "2",

}

RIS

TY - JOUR

T1 - The definition of the gas flow parameters in the shock layer near a thin variable form wing moving with a high variable velocity

AU - Bogatko, V. I.

AU - Kolton, G. A.

AU - Potekhina, E. A.

PY - 2002/1/1

Y1 - 2002/1/1

N2 - In thin shock layer method is applied to the problem under consideration. A vector of the wing velocity depends on the time. The head shock wave is considered to be joined to the surface of the body at least in an one point. The solution was written for the case when the vertical acceleration component is small.

AB - In thin shock layer method is applied to the problem under consideration. A vector of the wing velocity depends on the time. The head shock wave is considered to be joined to the surface of the body at least in an one point. The solution was written for the case when the vertical acceleration component is small.

UR - http://www.scopus.com/inward/record.url?scp=0036918799&partnerID=8YFLogxK

M3 - статья

AN - SCOPUS:0036918799

SP - 61

EP - 66

JO - ВЕСТНИК САНКТ-ПЕТЕРБУРГСКОГО УНИВЕРСИТЕТА. МАТЕМАТИКА. МЕХАНИКА. АСТРОНОМИЯ

JF - ВЕСТНИК САНКТ-ПЕТЕРБУРГСКОГО УНИВЕРСИТЕТА. МАТЕМАТИКА. МЕХАНИКА. АСТРОНОМИЯ

SN - 1025-3106

IS - 2

ER -

ID: 48962810