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Current Residence: Ukraine Favourite genre of music: Rock, symphonic metal Favourite style of art: pencil, 3D Operating System: Windows XP SP3 MP3 player of choice: AIMP Favourite cartoon character: Mikaze Honjou (本庄 美風) from Stratos 4 Personal Quote: Per aspera ad astra!
I completed translation my "lesson" at english, and posted it into my Livejournal for better comfortability I hope, that you find some interesting or useful at this work. Also, if you find some errors in translation (my english is not good) - write about it, and I will fix it. Part one: [link] Part two: [link] Enjoy it
Thanks Yes, i know about NACA airfoil, but this article very interesting I know about Profili 2 program, also - X-Foil Low Reynolds. These program alow you calculate Cl, Cd and pressure distributing at airfoil (also spanwise in XFLR).
i used some programs to create the naca section i want then import them in to a cad program so i could create the wing accurately, i think this was from when i was learning [link]
XFLR looks like a great program
haven't used any of those types of programs for awhile but last one i used was Fluent (i think)