ABSTRACT Unstructured grids are generated for multi-element airfoils and the corresponding Euler and Navier- Stokes flow solutions are obtained around NLR7301 and NLHP […]READ MORE
READ MORE -
ABSTRACT Multielement airfoil applications of a compressible Reynolds averaged Navier-Stokes Method “TURANS” and a second calculation method based on an efficient panel-boundary-layer coupled […]READ MORE
READ MORE -