The first file is a FreeCAD model of a 1m(nominal) 30P-30N wing and windtunnel along with a 2D CfdOF analysis object. I am starting the repository out with the following files so that others may use them to validate various meshing and simulation tools they may be using. Wolf Dynamics graciously provides a link to download the case file on their web page. Numerical study to assess sulfur hexafluoride as a medium for testing multi-element airfoils. 2002.Ĭomparative results from a CFD challenge over a 2D three-element high-lift airfoil. Progress in Aerospace Sciences, 38:145-180. Prediction of high lift: review of present CFD capability. They obtained a Cd of 2.237588 and a CL of 0.034598 versus the experimental values of 2.167089 and 0.033243 respectively.
In their validation case WD meshed and simulated a 30P-30N airfoil at a 0 degree AoA at a Reynolds number of 5,000,000 using the Spalart-Allmaras turbulence model. The impetus for this activity came from Wolf Dynamics 30P-30N validation case available here: This repository contains various resources necessary/helpful to validate the meshing and CFD simulation of a 30P-30N airfoil.
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