A Plasma-Actuator-Based Method to Generate a Supersonic Turbulent Boundary Layer Inflow Condition for Numerical Simulations
20th AIAA Computational Fluid Dynamics Conference
01.01.2011
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Numerical Simulations of Laminar-Turbulent Transition In Supersonic Boundary Layer
British Library Conference Proceedings | 2006
|Effects of inflow boundary layer on supersonic inlets
AIAA | 2024
|