High-Order Discontinuous Galerkin Mesh Resolved Turbulent Flow Simulations of a NACA 0012 Airfoil (Invited)
53rd AIAA Aerospace Sciences Meeting
01.01.2015
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2015
|Finite Element Solutions for Turbulent Flow over the NACA 0012 Airfoil
Online Contents | 2016
|Finite-Element Solutions for Turbulent Flow over the NACA 0012 Airfoil (Invited) (AIAA 2015-1531)
British Library Conference Proceedings | 2015
|