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About the unsteady hypersonic gas stream at flowing a thin wing with a variable form. / Bogatko, V. I.; Potekhina, E. A.

In: Vestnik Sankt-Peterburgskogo Universiteta. Ser 1. Matematika Mekhanika Astronomiya, No. 3, 01.07.1995, p. 73-78.

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

Harvard

Bogatko, VI & Potekhina, EA 1995, 'About the unsteady hypersonic gas stream at flowing a thin wing with a variable form', Vestnik Sankt-Peterburgskogo Universiteta. Ser 1. Matematika Mekhanika Astronomiya, no. 3, pp. 73-78.

APA

Bogatko, V. I., & Potekhina, E. A. (1995). About the unsteady hypersonic gas stream at flowing a thin wing with a variable form. Vestnik Sankt-Peterburgskogo Universiteta. Ser 1. Matematika Mekhanika Astronomiya, (3), 73-78.

Vancouver

Bogatko VI, Potekhina EA. About the unsteady hypersonic gas stream at flowing a thin wing with a variable form. Vestnik Sankt-Peterburgskogo Universiteta. Ser 1. Matematika Mekhanika Astronomiya. 1995 Jul 1;(3):73-78.

Author

Bogatko, V. I. ; Potekhina, E. A. / About the unsteady hypersonic gas stream at flowing a thin wing with a variable form. In: Vestnik Sankt-Peterburgskogo Universiteta. Ser 1. Matematika Mekhanika Astronomiya. 1995 ; No. 3. pp. 73-78.

BibTeX

@article{b422f46002c64a8ba8abdd11c101af57,
title = "About the unsteady hypersonic gas stream at flowing a thin wing with a variable form",
abstract = "The nonstationary problem of finding the parameters of the hypersonic gas stream beyond the front of the head shock wave resulting in flowing a thin wing with a variable form has been considered. The problem has been solved by means of the thin shock layer method. The gas flow in the shock layer has been described by the set of differential equations of gas dynamics with the boundary conditions on the head shock wave front and the wing surface. It has been assumed that the head shock wave has been joined to the front edge of the wing, and the attack angle has been not small. The corrections to a pressure, a longitudinal vector velocity component and an enthalpy have been obtained on the basis of solving the integrodifferential equations set.",
author = "Bogatko, {V. I.} and Potekhina, {E. A.}",
year = "1995",
month = jul,
day = "1",
language = "русский",
pages = "73--78",
journal = "ВЕСТНИК САНКТ-ПЕТЕРБУРГСКОГО УНИВЕРСИТЕТА. МАТЕМАТИКА. МЕХАНИКА. АСТРОНОМИЯ",
issn = "1025-3106",
publisher = "Издательство Санкт-Петербургского университета",
number = "3",

}

RIS

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T1 - About the unsteady hypersonic gas stream at flowing a thin wing with a variable form

AU - Bogatko, V. I.

AU - Potekhina, E. A.

PY - 1995/7/1

Y1 - 1995/7/1

N2 - The nonstationary problem of finding the parameters of the hypersonic gas stream beyond the front of the head shock wave resulting in flowing a thin wing with a variable form has been considered. The problem has been solved by means of the thin shock layer method. The gas flow in the shock layer has been described by the set of differential equations of gas dynamics with the boundary conditions on the head shock wave front and the wing surface. It has been assumed that the head shock wave has been joined to the front edge of the wing, and the attack angle has been not small. The corrections to a pressure, a longitudinal vector velocity component and an enthalpy have been obtained on the basis of solving the integrodifferential equations set.

AB - The nonstationary problem of finding the parameters of the hypersonic gas stream beyond the front of the head shock wave resulting in flowing a thin wing with a variable form has been considered. The problem has been solved by means of the thin shock layer method. The gas flow in the shock layer has been described by the set of differential equations of gas dynamics with the boundary conditions on the head shock wave front and the wing surface. It has been assumed that the head shock wave has been joined to the front edge of the wing, and the attack angle has been not small. The corrections to a pressure, a longitudinal vector velocity component and an enthalpy have been obtained on the basis of solving the integrodifferential equations set.

UR - http://www.scopus.com/inward/record.url?scp=0029336259&partnerID=8YFLogxK

M3 - статья

AN - SCOPUS:0029336259

SP - 73

EP - 78

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

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

SN - 1025-3106

IS - 3

ER -

ID: 48960876