High-Order Discontinuous Galerkin Mesh Resolved Turbulent Flow Simulations of a NACA 0012 Airfoil (Invited) (AIAA 2015-1529)
Aerospace sciences meeting
01.01.2015
25 pages
Aufsatz (Konferenz)
Englisch
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Finite-Element Solutions for Turbulent Flow over the NACA 0012 Airfoil (Invited) (AIAA 2015-1531)
British Library Conference Proceedings | 2015
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