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Instability of transonic flow over airfoils at singular freestream mach numbers. / Kuz'min, Alexander G.

2004. Paper presented at European Congress on Computational Methods in Applied Sciences and Engineering, ECCOMAS 2004, Jyvaskyla, Finland.

Research output: Contribution to conference › Paper › peer-review

Harvard

Kuz'min, AG 2004, 'Instability of transonic flow over airfoils at singular freestream mach numbers', Paper presented at European Congress on Computational Methods in Applied Sciences and Engineering, ECCOMAS 2004, Jyvaskyla, Finland, 24/07/04 - 28/07/04.

APA

Kuz'min, A. G. (2004). Instability of transonic flow over airfoils at singular freestream mach numbers. Paper presented at European Congress on Computational Methods in Applied Sciences and Engineering, ECCOMAS 2004, Jyvaskyla, Finland.

Vancouver

Kuz'min AG. Instability of transonic flow over airfoils at singular freestream mach numbers. 2004. Paper presented at European Congress on Computational Methods in Applied Sciences and Engineering, ECCOMAS 2004, Jyvaskyla, Finland.

Author

Kuz'min, Alexander G. / Instability of transonic flow over airfoils at singular freestream mach numbers. Paper presented at European Congress on Computational Methods in Applied Sciences and Engineering, ECCOMAS 2004, Jyvaskyla, Finland.

BibTeX

@conference{e11a50a984d94d109ab49a98256dc203,
title = "Instability of transonic flow over airfoils at singular freestream mach numbers",
abstract = "A few airfoil configurations whose curvature is small in the midchord region are considered. The structure of inviscid transonic flow over the airfoils is analyzed. The existence of singular values of the freestream Mach number and the incidence, which trigger off the abrupt restructuring of the flow, is demonstrated. A discontinuous dependence of the lift coefficient on the Mach number is discussed.",
keywords = "Freestream conditions, Instability, Inviscid flow, Lift coefficient, Local supersonic region, Nonuniqueness",
author = "Kuz'min, {Alexander G.}",
year = "2004",
language = "English",
note = "European Congress on Computational Methods in Applied Sciences and Engineering, ECCOMAS 2004 ; Conference date: 24-07-2004 Through 28-07-2004",

}

RIS

TY - CONF

T1 - Instability of transonic flow over airfoils at singular freestream mach numbers

AU - Kuz'min, Alexander G.

PY - 2004

Y1 - 2004

N2 - A few airfoil configurations whose curvature is small in the midchord region are considered. The structure of inviscid transonic flow over the airfoils is analyzed. The existence of singular values of the freestream Mach number and the incidence, which trigger off the abrupt restructuring of the flow, is demonstrated. A discontinuous dependence of the lift coefficient on the Mach number is discussed.

AB - A few airfoil configurations whose curvature is small in the midchord region are considered. The structure of inviscid transonic flow over the airfoils is analyzed. The existence of singular values of the freestream Mach number and the incidence, which trigger off the abrupt restructuring of the flow, is demonstrated. A discontinuous dependence of the lift coefficient on the Mach number is discussed.

KW - Freestream conditions

KW - Instability

KW - Inviscid flow

KW - Lift coefficient

KW - Local supersonic region

KW - Nonuniqueness

UR - http://www.scopus.com/inward/record.url?scp=84893455520&partnerID=8YFLogxK

M3 - Paper

AN - SCOPUS:84893455520

T2 - European Congress on Computational Methods in Applied Sciences and Engineering, ECCOMAS 2004

Y2 - 24 July 2004 through 28 July 2004

ER -

ID: 98581381