Pre-processed polars (by XFoil) for all the airfoils of the database at 20 predefined Reynolds numbers (from 30,000 to 500,000). Modification of airfoil thickness, camber and their application points Modification of airfoil external shape and camber line coordinates with the mouse, with CAD-like interface

Modification of airfoil coordinates in a visual way with the mouse, with CAD-like interface New airfoil creation by using external shape and camber line of different ones New airfoils creation by using upper and lower parts of different ones So you can then generate the polars and check the aerodynamic of your new wing. With this function you can generate the intermediate airfoils in a wing with different ones at root and tips. You can also define the mixing percentage. This lets you to create a new airfoil by mixing two selected from the database. PRO files.Īirfoils import from raster file (*.bmp, *.tif, etc).Īdvanced search by filtering based on library, name, thickness, camber and other geometrical parameters.Īutomatic computing for geometrical parameters.Ī new grid for an easy input of airfoil coordinates. Rib template, ribs template, ribs templates, foam cutting, trapezoidal or elliptical wing, new version,Īirfoils import-export from-to. KOOĪirfoil managing, airfoil printing, airfoil analysis, airfoil drawing,Īirfoils managing, airfoils printing, airfoils analysis, airfoils drawing,Ĭompufoil, airfoils archive, airfoil archive, NACA, eppler, SD, selig, mh, hq,Ĭamber, thickness, chord, wing, wing airfoil, wings, wing airfoils, process, elaborateĪirfoil processing, airfoils processing, process airfoil, process airfoils, polar analysis, analize polars,īest software, great software, free download, free update, no cost, rib generation, ribs generation, Print printing preview, modify airfoils, process airfoils, DAT COR KOO import export. Momento lift momentum drag resistenza portanza profili2, profili 2.0, profili 2.1, profiliv2, disegno stampa.

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