A supersonic viscous gas flow past a blunt cylindrical body bounded at its ends by parallel plates

The paper presents the results of calculations of a supersonic laminar flow past a cylindrical body located between parallel horizontal walls (plates). The free-stream Mach number M = 5. Calculations were carried out for various values of the geometric factor χ defined as the ratio of the distance b...

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Main Authors: Kolesnik Elizaveta, Babich Elena, Smirnov Evgeny
Format: Article
Language:English
Published: Peter the Great St.Petersburg Polytechnic University 2025-03-01
Series:St. Petersburg Polytechnical University Journal: Physics and Mathematics
Subjects:
Online Access:https://physmath.spbstu.ru/article/2025.78.02/
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author Kolesnik Elizaveta
Babich Elena
Smirnov Evgeny
author_facet Kolesnik Elizaveta
Babich Elena
Smirnov Evgeny
author_sort Kolesnik Elizaveta
collection DOAJ
description The paper presents the results of calculations of a supersonic laminar flow past a cylindrical body located between parallel horizontal walls (plates). The free-stream Mach number M = 5. Calculations were carried out for various values of the geometric factor χ defined as the ratio of the distance between the walls to the blunt diameter of the leading edge of the body, the ratio varying from 2 to infinity. Decreasing the distance between the walls was shown to lead to a shift of the separated shock closer to the streamlined body, and to an increase in the thickness of the separation region. In the case of χ = 2 a nonstationary self-oscillatory flow regime characterized by strong oscillations of the separated shock wave was realized.
format Article
id doaj-art-3555cff4658b4d38b61ab59e1f47b8e5
institution OA Journals
issn 2405-7223
language English
publishDate 2025-03-01
publisher Peter the Great St.Petersburg Polytechnic University
record_format Article
series St. Petersburg Polytechnical University Journal: Physics and Mathematics
spelling doaj-art-3555cff4658b4d38b61ab59e1f47b8e52025-08-20T01:50:50ZengPeter the Great St.Petersburg Polytechnic UniversitySt. Petersburg Polytechnical University Journal: Physics and Mathematics2405-72232025-03-0118110.18721/JPM.1810220714726A supersonic viscous gas flow past a blunt cylindrical body bounded at its ends by parallel platesKolesnik Elizaveta0https://orcid.org/0000-0002-6308-733XBabich Elena1https://orcid.org/0000-0003-1442-4886Smirnov Evgeny2https://orcid.org/0000-0002-7218-6372Peter the Great St. Petersburg Polytechnic UniversityPeter the Great St. Petersburg Polytechnic UniversityPeter the Great St. Petersburg Polytechnic UniversityThe paper presents the results of calculations of a supersonic laminar flow past a cylindrical body located between parallel horizontal walls (plates). The free-stream Mach number M = 5. Calculations were carried out for various values of the geometric factor χ defined as the ratio of the distance between the walls to the blunt diameter of the leading edge of the body, the ratio varying from 2 to infinity. Decreasing the distance between the walls was shown to lead to a shift of the separated shock closer to the streamlined body, and to an increase in the thickness of the separation region. In the case of χ = 2 a nonstationary self-oscillatory flow regime characterized by strong oscillations of the separated shock wave was realized.https://physmath.spbstu.ru/article/2025.78.02/high-speed flownumerical simulationinternal separated flowviscous-inviscid interactionhorseshoe vortex
spellingShingle Kolesnik Elizaveta
Babich Elena
Smirnov Evgeny
A supersonic viscous gas flow past a blunt cylindrical body bounded at its ends by parallel plates
St. Petersburg Polytechnical University Journal: Physics and Mathematics
high-speed flow
numerical simulation
internal separated flow
viscous-inviscid interaction
horseshoe vortex
title A supersonic viscous gas flow past a blunt cylindrical body bounded at its ends by parallel plates
title_full A supersonic viscous gas flow past a blunt cylindrical body bounded at its ends by parallel plates
title_fullStr A supersonic viscous gas flow past a blunt cylindrical body bounded at its ends by parallel plates
title_full_unstemmed A supersonic viscous gas flow past a blunt cylindrical body bounded at its ends by parallel plates
title_short A supersonic viscous gas flow past a blunt cylindrical body bounded at its ends by parallel plates
title_sort supersonic viscous gas flow past a blunt cylindrical body bounded at its ends by parallel plates
topic high-speed flow
numerical simulation
internal separated flow
viscous-inviscid interaction
horseshoe vortex
url https://physmath.spbstu.ru/article/2025.78.02/
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