Open AccessA stability based transition prediction criterion for up to Mach 8 hypersonic flows
Author(s) -
Jean Perraud,
Jean-Philippe Brazier
Publication year - 2019
Publication title -
hal (le centre pour la communication scientifique directe)
Language(s) - English
Resource type - Conference proceedings
Subject(s) - mach number , adiabatic wall , boundary layer , mechanics , transonic , hypersonic speed , laminar flow , turbulent prandtl number , adiabatic process , reynolds averaged navier–stokes equations , work (physics) , laminar turbulent transition , turbulence , hypersonic flight , physics , computer science , aerodynamics , thermodynamics , reynolds number , nusselt number
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