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The structural instability of transonic flow associated with amalgamation/splitting of supersonic regions. / Kuz'min, Alexander G.; Ivanova, Alexandra V.

в: Theoretical and Computational Fluid Dynamics, Том 18, № 5, 11.2004, стр. 335-344.

Результаты исследований: Научные публикации в периодических изданияхстатьяРецензирование

Harvard

Kuz'min, AG & Ivanova, AV 2004, 'The structural instability of transonic flow associated with amalgamation/splitting of supersonic regions', Theoretical and Computational Fluid Dynamics, Том. 18, № 5, стр. 335-344. https://doi.org/10.1007/s00162-004-0145-1

APA

Vancouver

Author

Kuz'min, Alexander G. ; Ivanova, Alexandra V. / The structural instability of transonic flow associated with amalgamation/splitting of supersonic regions. в: Theoretical and Computational Fluid Dynamics. 2004 ; Том 18, № 5. стр. 335-344.

BibTeX

@article{108c144679c144ef8106784baaef6a6c,
title = "The structural instability of transonic flow associated with amalgamation/splitting of supersonic regions",
abstract = "We study inviscid transonic flow in a channel with a bump modeling an airfoil at zero incidence. A few simple bump configurations are considered. Numerical simulations show the existence of singular free-stream Mach numbers, which trigger the splitting/amalgamation of local supersonic regions. An analysis of this phenomenon contributes to the understanding of the nonuniqueness of transonic solutions at certain free-stream conditions.",
keywords = "Instability, Interaction, Local supersonic regions, Oblique shocks",
author = "Kuz'min, {Alexander G.} and Ivanova, {Alexandra V.}",
year = "2004",
month = nov,
doi = "10.1007/s00162-004-0145-1",
language = "English",
volume = "18",
pages = "335--344",
journal = "Theoretical and Computational Fluid Dynamics",
issn = "0935-4964",
publisher = "Springer Nature",
number = "5",

}

RIS

TY - JOUR

T1 - The structural instability of transonic flow associated with amalgamation/splitting of supersonic regions

AU - Kuz'min, Alexander G.

AU - Ivanova, Alexandra V.

PY - 2004/11

Y1 - 2004/11

N2 - We study inviscid transonic flow in a channel with a bump modeling an airfoil at zero incidence. A few simple bump configurations are considered. Numerical simulations show the existence of singular free-stream Mach numbers, which trigger the splitting/amalgamation of local supersonic regions. An analysis of this phenomenon contributes to the understanding of the nonuniqueness of transonic solutions at certain free-stream conditions.

AB - We study inviscid transonic flow in a channel with a bump modeling an airfoil at zero incidence. A few simple bump configurations are considered. Numerical simulations show the existence of singular free-stream Mach numbers, which trigger the splitting/amalgamation of local supersonic regions. An analysis of this phenomenon contributes to the understanding of the nonuniqueness of transonic solutions at certain free-stream conditions.

KW - Instability

KW - Interaction

KW - Local supersonic regions

KW - Oblique shocks

UR - http://www.scopus.com/inward/record.url?scp=10644262222&partnerID=8YFLogxK

U2 - 10.1007/s00162-004-0145-1

DO - 10.1007/s00162-004-0145-1

M3 - Article

AN - SCOPUS:10644262222

VL - 18

SP - 335

EP - 344

JO - Theoretical and Computational Fluid Dynamics

JF - Theoretical and Computational Fluid Dynamics

SN - 0935-4964

IS - 5

ER -

ID: 98581648