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Interaction of a shock wave with the sonic line. / Kuz'min, A. G.

IUTAM Symposium Transsonicum IV. ed. / H. SOBIECZKY. 2003. p. 13-18 (Fluid Mechanics and its Applications; Vol. 73).

Research output: Chapter in Book/Report/Conference proceeding › Chapter › peer-review

Harvard

Kuz'min, AG 2003, Interaction of a shock wave with the sonic line. in H SOBIECZKY (ed.), IUTAM Symposium Transsonicum IV. Fluid Mechanics and its Applications, vol. 73, pp. 13-18. https://doi.org/10.1007/978-94-010-0017-8_3

APA

Kuz'min, A. G. (2003). Interaction of a shock wave with the sonic line. In H. SOBIECZKY (Ed.), IUTAM Symposium Transsonicum IV (pp. 13-18). (Fluid Mechanics and its Applications; Vol. 73). https://doi.org/10.1007/978-94-010-0017-8_3

Vancouver

Kuz'min AG. Interaction of a shock wave with the sonic line. In SOBIECZKY H, editor, IUTAM Symposium Transsonicum IV. 2003. p. 13-18. (Fluid Mechanics and its Applications). https://doi.org/10.1007/978-94-010-0017-8_3

Author

Kuz'min, A. G. / Interaction of a shock wave with the sonic line. IUTAM Symposium Transsonicum IV. editor / H. SOBIECZKY. 2003. pp. 13-18 (Fluid Mechanics and its Applications).

BibTeX

@inbook{a4da120674f14f9f93dcc35838d11477,
title = "Interaction of a shock wave with the sonic line",
abstract = "The paper addresses patterns of interaction of shock waves with the sonic line. The incident shocks are formed by either a small curvature of an airfoil arc, or a small step in its contour, or a short bump superposed on the airfoil. We analyse the structure of inviscid steady flow and discuss its instability at certain boundary conditions.",
author = "Kuz'min, {A. G.}",
year = "2003",
month = dec,
day = "1",
doi = "10.1007/978-94-010-0017-8_3",
language = "English",
isbn = "1402016085",
series = "Fluid Mechanics and its Applications",
pages = "13--18",
editor = "H. SOBIECZKY",
booktitle = "IUTAM Symposium Transsonicum IV",

}

RIS

TY - CHAP

T1 - Interaction of a shock wave with the sonic line

AU - Kuz'min, A. G.

PY - 2003/12/1

Y1 - 2003/12/1

N2 - The paper addresses patterns of interaction of shock waves with the sonic line. The incident shocks are formed by either a small curvature of an airfoil arc, or a small step in its contour, or a short bump superposed on the airfoil. We analyse the structure of inviscid steady flow and discuss its instability at certain boundary conditions.

AB - The paper addresses patterns of interaction of shock waves with the sonic line. The incident shocks are formed by either a small curvature of an airfoil arc, or a small step in its contour, or a short bump superposed on the airfoil. We analyse the structure of inviscid steady flow and discuss its instability at certain boundary conditions.

UR - http://www.scopus.com/inward/record.url?scp=84859715685&partnerID=8YFLogxK

U2 - 10.1007/978-94-010-0017-8_3

DO - 10.1007/978-94-010-0017-8_3

M3 - Chapter

AN - SCOPUS:84859715685

SN - 1402016085

SN - 9781402016080

T3 - Fluid Mechanics and its Applications

SP - 13

EP - 18

BT - IUTAM Symposium Transsonicum IV

A2 - SOBIECZKY, H.

ER -

ID: 38435280