Standard

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

In: Vestnik Sankt-Peterburgskogo Universiteta. Ser 1. Matematika Mekhanika Astronomiya, No. 3, 01.01.2002, p. 69-73.

Research output: Contribution to journal › Article › peer-review

Harvard

Bogatko, VI, Kolton, GA & Potekhina, EA 2002, 'The definition of the gas flow parameters in the shock layer near a thin finite span wing moving with a high variable velocity', Vestnik Sankt-Peterburgskogo Universiteta. Ser 1. Matematika Mekhanika Astronomiya, no. 3, pp. 69-73.

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 finite span wing moving with a high variable velocity. Vestnik Sankt-Peterburgskogo Universiteta. Ser 1. Matematika Mekhanika Astronomiya, (3), 69-73.

Vancouver

Bogatko VI, Kolton GA, Potekhina EA. The definition of the gas flow parameters in the shock layer near a thin finite span wing moving with a high variable velocity. Vestnik Sankt-Peterburgskogo Universiteta. Ser 1. Matematika Mekhanika Astronomiya. 2002 Jan 1;(3):69-73.

Author

Bogatko, V. I. ; Kolton, G. A. ; Potekhina, E. A. / The definition of the gas flow parameters in the shock layer near a thin finite span wing moving with a high variable velocity. In: Vestnik Sankt-Peterburgskogo Universiteta. Ser 1. Matematika Mekhanika Astronomiya. 2002 ; No. 3. pp. 69-73.

BibTeX

@article{ca69bebe3b2f4410bf81db92eb348fe1,
title = "The definition of the gas flow parameters in the shock layer near a thin finite span wing moving with a high variable velocity",
abstract = "The 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 as joined to the front edge of the wing. The solution is written in the finite form.",
author = "Bogatko, {V. I.} and Kolton, {G. A.} and Potekhina, {E. A.}",
year = "2002",
month = jan,
day = "1",
language = "русский",
pages = "69--73",
journal = "ВЕСТНИК САНКТ-ПЕТЕРБУРГСКОГО УНИВЕРСИТЕТА. МАТЕМАТИКА. МЕХАНИКА. АСТРОНОМИЯ",
issn = "1025-3106",
publisher = "Издательство Санкт-Петербургского университета",
number = "3",

}

RIS

TY - JOUR

T1 - The definition of the gas flow parameters in the shock layer near a thin finite span 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 - The 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 as joined to the front edge of the wing. The solution is written in the finite form.

AB - The 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 as joined to the front edge of the wing. The solution is written in the finite form.

UR - http://www.scopus.com/inward/record.url?scp=0038677722&partnerID=8YFLogxK

M3 - статья

AN - SCOPUS:0038677722

SP - 69

EP - 73

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

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

SN - 1025-3106

IS - 3

ER -

ID: 48962881