The influence of a flap on the two-dimensional NACA airfoil in viscous ground-effect flow is numerically investigated in this study. The computational method consists of a steady-state, incompressible, finite volume method utilizing the Spalart-Allmaras turbulence holbrook-ne.com by: The Computer-Aided Design ("CAD") files and all associated content posted to this website are created, uploaded, managed and owned by third party users. The NACA staff utilize a power point presentation at the workshop. This provides an outline for the presentation, which is supplemented by the staff and the questions of the participants. You must attend a workshop before you can participate in the NACA program.
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