Redistribution of Energy during Interaction of a Shock Wave with a Temperature Layered Plasma Region at Hypersonic Speeds

The paper is devoted to the problem of the interaction between a shock wave and a thermally stratified energy source for the purpose of supersonic/hypersonic flow control realization. The effect of the thermally stratified energy source on a shock wave with the Mach number in the range of 6–12 is re...

Descripción completa

Guardado en:
Detalles Bibliográficos
Autores principales: O. A. Azarova, T. A. Lapushkina, K. V. Krasnobaev, O. V. Kravchenko
Formato: article
Lenguaje:EN
Publicado: MDPI AG 2021
Materias:
Acceso en línea:https://doaj.org/article/dc2fb9dfbd81439cb3a0a5da087c5cdc
Etiquetas: Agregar Etiqueta
Sin Etiquetas, Sea el primero en etiquetar este registro!
id oai:doaj.org-article:dc2fb9dfbd81439cb3a0a5da087c5cdc
record_format dspace
spelling oai:doaj.org-article:dc2fb9dfbd81439cb3a0a5da087c5cdc2021-11-25T15:57:19ZRedistribution of Energy during Interaction of a Shock Wave with a Temperature Layered Plasma Region at Hypersonic Speeds10.3390/aerospace81103262226-4310https://doaj.org/article/dc2fb9dfbd81439cb3a0a5da087c5cdc2021-11-01T00:00:00Zhttps://www.mdpi.com/2226-4310/8/11/326https://doaj.org/toc/2226-4310The paper is devoted to the problem of the interaction between a shock wave and a thermally stratified energy source for the purpose of supersonic/hypersonic flow control realization. The effect of the thermally stratified energy source on a shock wave with the Mach number in the range of 6–12 is researched numerically based on the Navier-Stokes system of equations. Redistribution of specific internal energy and volume density of kinetic energy behind the wave front is investigated. Multiple manifestations of the Richtmyer-Meshkov instability has been obtained which has caused the blurring and disappearance of shock wave and contact discontinuity fronts in density fields. A study of the efficiency of using a stratified energy source instead of a homogeneous one with the same value of the full energy is carried out. The agreement with the available experimental data for the shock wave Mach number 6 has been obtained.O. A. AzarovaT. A. LapushkinaK. V. KrasnobaevO. V. KravchenkoMDPI AGarticlethermally stratified energy sourceshock wavehypersonic speedsglow dischargeionization instabilityRichtmyer-Meshkov instabilityMotor vehicles. Aeronautics. AstronauticsTL1-4050ENAerospace, Vol 8, Iss 326, p 326 (2021)
institution DOAJ
collection DOAJ
language EN
topic thermally stratified energy source
shock wave
hypersonic speeds
glow discharge
ionization instability
Richtmyer-Meshkov instability
Motor vehicles. Aeronautics. Astronautics
TL1-4050
spellingShingle thermally stratified energy source
shock wave
hypersonic speeds
glow discharge
ionization instability
Richtmyer-Meshkov instability
Motor vehicles. Aeronautics. Astronautics
TL1-4050
O. A. Azarova
T. A. Lapushkina
K. V. Krasnobaev
O. V. Kravchenko
Redistribution of Energy during Interaction of a Shock Wave with a Temperature Layered Plasma Region at Hypersonic Speeds
description The paper is devoted to the problem of the interaction between a shock wave and a thermally stratified energy source for the purpose of supersonic/hypersonic flow control realization. The effect of the thermally stratified energy source on a shock wave with the Mach number in the range of 6–12 is researched numerically based on the Navier-Stokes system of equations. Redistribution of specific internal energy and volume density of kinetic energy behind the wave front is investigated. Multiple manifestations of the Richtmyer-Meshkov instability has been obtained which has caused the blurring and disappearance of shock wave and contact discontinuity fronts in density fields. A study of the efficiency of using a stratified energy source instead of a homogeneous one with the same value of the full energy is carried out. The agreement with the available experimental data for the shock wave Mach number 6 has been obtained.
format article
author O. A. Azarova
T. A. Lapushkina
K. V. Krasnobaev
O. V. Kravchenko
author_facet O. A. Azarova
T. A. Lapushkina
K. V. Krasnobaev
O. V. Kravchenko
author_sort O. A. Azarova
title Redistribution of Energy during Interaction of a Shock Wave with a Temperature Layered Plasma Region at Hypersonic Speeds
title_short Redistribution of Energy during Interaction of a Shock Wave with a Temperature Layered Plasma Region at Hypersonic Speeds
title_full Redistribution of Energy during Interaction of a Shock Wave with a Temperature Layered Plasma Region at Hypersonic Speeds
title_fullStr Redistribution of Energy during Interaction of a Shock Wave with a Temperature Layered Plasma Region at Hypersonic Speeds
title_full_unstemmed Redistribution of Energy during Interaction of a Shock Wave with a Temperature Layered Plasma Region at Hypersonic Speeds
title_sort redistribution of energy during interaction of a shock wave with a temperature layered plasma region at hypersonic speeds
publisher MDPI AG
publishDate 2021
url https://doaj.org/article/dc2fb9dfbd81439cb3a0a5da087c5cdc
work_keys_str_mv AT oaazarova redistributionofenergyduringinteractionofashockwavewithatemperaturelayeredplasmaregionathypersonicspeeds
AT talapushkina redistributionofenergyduringinteractionofashockwavewithatemperaturelayeredplasmaregionathypersonicspeeds
AT kvkrasnobaev redistributionofenergyduringinteractionofashockwavewithatemperaturelayeredplasmaregionathypersonicspeeds
AT ovkravchenko redistributionofenergyduringinteractionofashockwavewithatemperaturelayeredplasmaregionathypersonicspeeds
_version_ 1718413410153005056