Publication Date:
2013-08-31
Description:
Mesh generation procedures as well as solution algorithms for solving the Euler and Navier-Stokes equations on unstructured meshes are presented. The solution algorithms discussed utilize approximate Riemann solver, upwind differencing to achieve high spatial accuracy. Numerical results for Euler flow over single and multi-element airfoils are presented.
Keywords:
AERODYNAMICS
Type:
NASA Computational Fluid Dynamics Conference. Volume 2: Sessions 7-12; p 379-393
Format:
application/pdf