Direct numerical simulation of flow separation around a NACA 0012 airfoil
- 1 November 2005
- journal article
- Published by Elsevier BV in Computers & Fluids
- Vol. 34 (9), 1096-1114
- https://doi.org/10.1016/j.compfluid.2004.09.003
Abstract
No abstract availableKeywords
This publication has 13 references indexed in Scilit:
- Direct numerical simulation of ‘short’ laminar separation bubbles with turbulent reattachmentJournal of Fluid Mechanics, 2000
- Mechanisms of transition and heat transfer in a separation bubbleJournal of Fluid Mechanics, 2000
- Direct numerical simulation of three-dimensional flow around a delta wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2000
- Further development of a Navier-Stokes solution procedure based on higher-order formulasPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1999
- Direct Numerical Simulation of Boundary-Layer Receptivity for Subsonic Flow Around AirfoilPublished by Springer Science and Business Media LLC ,1999
- Boundary layer development after a separated regionJournal of Fluid Mechanics, 1998
- PARABOLIZED STABILITY EQUATIONSAnnual Review of Fluid Mechanics, 1997
- Compact finite difference schemes with spectral-like resolutionJournal of Computational Physics, 1992
- Linear and nonlinear stability of the Blasius boundary layerJournal of Fluid Mechanics, 1992
- Boundary conditions for direct simulations of compressible viscous flowsJournal of Computational Physics, 1992