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Polynomial Gridgeneration Wizard for creating structured CFD-grids around airfoils with blunt and sharp trailing edges This version is tested for Matlab 8.6.0.267246 (R2015b) and Matlab 9.4.0.813654 (R2018a) The package contains: the Matlab beta-version of the code (ready-to-run) an example for a NACA 4412 profile with a sharp trailing edge (Grid_NACA4412_sharp_Style1) an example for a NACA 4412 profile with a blunt trailing edge (Grid_NACA4412_blunt_Style1) an example for optimised eta-gridlines according to the appendix A in the attached paper (Grid_NACA4412_sharp_Style3) a raw geometry of a cut-off NACA profile that can be read in by the code (Naca0012_cutoff_C1) The version 1.0.0 is supposed to contain the following features: parallelised 2D grid generation optimised modular structure open-source version written in Python (www.Jupyter.org) gridline-intersection check Release_Draft_ICCFD10.pdf
sharp-trailing-edges, blunt-trailing-edges, CFD, airfoil, grid-generation
sharp-trailing-edges, blunt-trailing-edges, CFD, airfoil, grid-generation
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