High-Order Discontinuous Galerkin Mesh Resolved Turbulent Flow Simulations of a NACA 0012 Airfoil (Invited) (AIAA 2015-1529)
Aerospace sciences meeting
2015-01-01
25 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Finite-Element Solutions for Turbulent Flow over the NACA 0012 Airfoil (Invited) (AIAA 2015-1531)
British Library Conference Proceedings | 2015
|British Library Conference Proceedings | 2015
|