Advance in LES Modelling: Effect of the Turbulent Schmidt Number on Supersonic Regime
43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
01.01.2007
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Advance in LES Modelling: Effect of the Turbulent Schmidt Number on Supersonic Regime AIAA Paper
British Library Conference Proceedings | 2007
|AIAA-2007-1312 EFFECT OF THE TURBULENT SCHMIDT ON SUPERSONIC REGIME
British Library Conference Proceedings | 2007
|LES of Supersonic combustion with a variable Turbulent Schmidt Number
British Library Conference Proceedings | 2008
|Simulation of Supersonic Combustion Using Variable Turbulent Prandtl/Schmidt Number Formulation
British Library Conference Proceedings | 2006
|