NACA 5 digit Airfoil Generator 1.0

"naca5gen.m" Generates the NACA 5 digit airfoil coordinates with desired no. of panels (line elements) on it. FEATURES: *Accurate coordinate generation with the required precision *Option to generate closed or open Trailing Edge *Additional separate outputs for camber line, upper surface and lower surface *A tst (test) file included INPUTS:[1] NACA 5 digit designation (eg. '23012')[2] No of panels (line elements) PER SIDE (upper/lower)[3] Type of chord station spacing (Half cosine spacing / Uniform spacing) OUTPUTS:[1] One can plot the generated airfoil, camber line and the leading edge circle by setting an option input wantPlot=1[2] A data file can be generated by setting the option input wantFile=1 EXTENSION:Being a function, the airfoil generator can be called several times from a loop to generate any number of airfoil data files.

Requirements:	No special requirements
Platforms:	Matlab
Keyword:	039230120392 No,  Accurate Coordinate,  Additional Separate,  Airfoil Camber,  Airfoil Coordinates,  Airfoil Data,  Airfoil Generator,  And The,  Lower,  Number,  Option,  Required,  Surface L,  Test File Included,  Tst Test File,  Uniform Spacing Outputs,  Upper Surface
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