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Viscous effects of shock reflection hysteresis in steady supersonic flows

Author
YUAN TAO1 ; XIAOQIANG FAN1 ; YILONG ZHAO1
[1] Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha 410073, China
Source

Journal of fluid mechanics. 2014, Vol 759, pp 134-148, 15 p ; ref : 3/4 p

CODEN
JFLSA7
ISSN
0022-1120
Scientific domain
Mechanics acoustics
Publisher
Cambridge University Press, Cambridge
Publication country
United Kingdom
Document type
Article
Language
English
Keyword (fr)
Couche limite Décollement couche limite Ecoulement supersonique Etude expérimentale Fluide visqueux Interaction Onde choc Réflexion onde Simulation numérique Transition laminaire turbulente 4727C 4740N
Keyword (en)
Boundary layers Boundary layer separation Supersonic flow Experimental study Viscous fluids Interactions Shock waves Wave reflection Digital simulation Turbulent laminar transition
Keyword (es)
Despegadura capa límite Reflexión onda
Classification
Pascal
001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40G Fluid dynamics / 001B40G27 Turbulent flows, convection, and heat transfer / 001B40G27C Transition to turbulence

Pascal
001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40G Fluid dynamics / 001B40G40 Compressible flows; shock and detonation phenomena / 001B40G40N Shock-wave interactions and shock effects

Discipline
Physics : fluid mechanics
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
29041447

Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS

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