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Transonic region formation at the thermal and gas-dynamic action on a supersonic duct flow. / Zamuraev, V. P.; Kalinina, A. P.

в: Thermophysics and Aeromechanics, Том 25, № 1, 01.01.2018, стр. 149-152.

Результаты исследований: Научные публикации в периодических изданияхстатьяРецензирование

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Zamuraev VP, Kalinina AP. Transonic region formation at the thermal and gas-dynamic action on a supersonic duct flow. Thermophysics and Aeromechanics. 2018 янв. 1;25(1):149-152. doi: 10.1134/S0869864318010146

Author

Zamuraev, V. P. ; Kalinina, A. P. / Transonic region formation at the thermal and gas-dynamic action on a supersonic duct flow. в: Thermophysics and Aeromechanics. 2018 ; Том 25, № 1. стр. 149-152.

BibTeX

@article{e8d0caa9abb14593b24a777f6b3e9568,
title = "Transonic region formation at the thermal and gas-dynamic action on a supersonic duct flow",
abstract = "The control simultaneous action of a jet and near-wall energy sources on the shockwave structure of a superso-nic flow in the axisymmetric and planar ducts is studied for the purpose of creating a transonic region. The regimes with an extended transonic region are obtained.",
keywords = "duct, Euler and Navier−Stokes equations, jet, near-wall energy sources, supersonic flow",
author = "Zamuraev, {V. P.} and Kalinina, {A. P.}",
year = "2018",
month = jan,
day = "1",
doi = "10.1134/S0869864318010146",
language = "English",
volume = "25",
pages = "149--152",
journal = "Thermophysics and Aeromechanics",
issn = "0869-8643",
publisher = "PLEIADES PUBLISHING INC",
number = "1",

}

RIS

TY - JOUR

T1 - Transonic region formation at the thermal and gas-dynamic action on a supersonic duct flow

AU - Zamuraev, V. P.

AU - Kalinina, A. P.

PY - 2018/1/1

Y1 - 2018/1/1

N2 - The control simultaneous action of a jet and near-wall energy sources on the shockwave structure of a superso-nic flow in the axisymmetric and planar ducts is studied for the purpose of creating a transonic region. The regimes with an extended transonic region are obtained.

AB - The control simultaneous action of a jet and near-wall energy sources on the shockwave structure of a superso-nic flow in the axisymmetric and planar ducts is studied for the purpose of creating a transonic region. The regimes with an extended transonic region are obtained.

KW - duct

KW - Euler and Navier−Stokes equations

KW - jet

KW - near-wall energy sources

KW - supersonic flow

UR - http://www.scopus.com/inward/record.url?scp=85045413476&partnerID=8YFLogxK

U2 - 10.1134/S0869864318010146

DO - 10.1134/S0869864318010146

M3 - Article

AN - SCOPUS:85045413476

VL - 25

SP - 149

EP - 152

JO - Thermophysics and Aeromechanics

JF - Thermophysics and Aeromechanics

SN - 0869-8643

IS - 1

ER -

ID: 12561012