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XFOIL
XFOIL is an interactive program for the design and analysis of subsonic isolated airfoils. Given the coordinates specifying the shape of a 2D airfoil, Reynolds and Mach numbers, XFOIL can calculate the pressure distribution on the airfoil and hence lift and drag characteristics. The program also allows ''inverse design'' - it will vary an airfoil shape to achieve the desired parameters. It is released under the GNU GPL. ==History==
XFOIL was first developed by Mark Drela at MIT as a design tool for the MIT Daedalus project in the 1980s.〔http://web.mit.edu/aeroastro/news/magazine/aeroastro-no3/2006drela.html〕 It was further developed in collaboration with Harold Youngren. The current version is 6.99, released in December 2013. Despite its vintage, it is still widely used.〔http://www.aoe.vt.edu/~mason/Mason_f/MRsoft.html〕 XFOIL is written in FORTRAN.
抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)』 ■ウィキペディアで「XFOIL」の詳細全文を読む
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