Impact of High-Temperature Effects on Shock Inclination Angle in Super- and Hypersonic Flow around Sharp Cone

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Impact of High-Temperature Effects on Shock Inclination Angle in Super- and Hypersonic Flow around Sharp Cone. / Volkov, K. N.; Emel’yanov, V. N.; Karpenko, A. G.; Tolstoguzov, S. S.

в: Russian Aeronautics, Том 64, № 3, 07.2021, стр. 466-475.

Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование

Author

Volkov, K. N. ; Emel’yanov, V. N. ; Karpenko, A. G. ; Tolstoguzov, S. S. / Impact of High-Temperature Effects on Shock Inclination Angle in Super- and Hypersonic Flow around Sharp Cone. в: Russian Aeronautics. 2021 ; Том 64, № 3. стр. 466-475.

BibTeX

@article{e2a3a6b278c047569022f0b3b98bfa68,

title = "Impact of High-Temperature Effects on Shock Inclination Angle in Super- and Hypersonic Flow around Sharp Cone",

abstract = "Abstract: Numerical simulation of a super- and hypersonic flow of an inviscid gas around a sharp cone is performed taking into account high-temperature effects. The numerical implementation of a computational procedure designed to find stationary solutions of the gas dynamics equations describing flows around a cone with the real gas properties is carried out.",

keywords = "aerodynamics, cone, cone flow, real gas, shock wave, supersonic flow",

author = "Volkov, {K. N.} and Emel{\textquoteright}yanov, {V. N.} and Karpenko, {A. G.} and Tolstoguzov, {S. S.}",

note = "Publisher Copyright: {\textcopyright} 2021, Allerton Press, Inc.",

year = "2021",

month = jul,

doi = "10.3103/S1068799821030132",

language = "English",

volume = "64",

pages = "466--475",

journal = "Russian Aeronautics",

issn = "1068-7998",

publisher = "Allerton Press, Inc.",

number = "3",

}

RIS

TY - JOUR

T1 - Impact of High-Temperature Effects on Shock Inclination Angle in Super- and Hypersonic Flow around Sharp Cone

AU - Volkov, K. N.

AU - Emel’yanov, V. N.

AU - Karpenko, A. G.

AU - Tolstoguzov, S. S.

PY - 2021/7

Y1 - 2021/7

N2 - Abstract: Numerical simulation of a super- and hypersonic flow of an inviscid gas around a sharp cone is performed taking into account high-temperature effects. The numerical implementation of a computational procedure designed to find stationary solutions of the gas dynamics equations describing flows around a cone with the real gas properties is carried out.

AB - Abstract: Numerical simulation of a super- and hypersonic flow of an inviscid gas around a sharp cone is performed taking into account high-temperature effects. The numerical implementation of a computational procedure designed to find stationary solutions of the gas dynamics equations describing flows around a cone with the real gas properties is carried out.

KW - aerodynamics

KW - cone

KW - cone flow

KW - real gas

KW - shock wave

KW - supersonic flow

UR - http://www.scopus.com/inward/record.url?scp=85121457616&partnerID=8YFLogxK

U2 - 10.3103/S1068799821030132

DO - 10.3103/S1068799821030132

M3 - Article

AN - SCOPUS:85121457616

VL - 64

SP - 466

EP - 475

JO - Russian Aeronautics

JF - Russian Aeronautics

SN - 1068-7998

IS - 3

ER -

ID: 92536768