Translations:Macro AeroFoil/28/en


 * 1) For the NACA airfoils, the last two digits (combined) cannot have a value of zero; thickness cannot be a zero value.
 * 2) The NACA 5-digit airfoils are limited to the following models ('XX' denotes the last two digits, thickness, of the airfoil) :
 * 3) * 210XX
 * 4) * 220XX
 * 5) * 221XX
 * 6) * 230XX
 * 7) * 231XX
 * 8) * 240XX
 * 9) * 241XX
 * 10) * 250XX
 * 11) * 251XX
 * 12) For curve functions, only use the preset characters and functions.
 * 13) For curve functions, $$2 * x$$ is correct, whereas $$2x$$ is incorrect.
 * 14) For curve functions, $$y = f(x)$$ ranges from 0 to 1, both inclusive.
 * 15) For curve functions, the trigonometric theta is in degrees (&theta; &deg;)
 * 16) For curve functions, the trigonometric theta ranges from 0&deg; to 360&deg;, subject to computational limits.
 * 17) Curves or points that are intersecting between 0 and 1, both exclusive, will return an error.
 * 18) Curves or points that contain the bottom airfoil data cannot be mirrored
 * 19) For file imports, it is suggested to leave the line, row, and column numbers to their default values, unless you are well-informed.
 * 20) Increasing the refine and quantity parameters increases the computation time and resources.
 * 21) Absolute chord length, in millimetres, cannot be less than 1mm.