![]() ![]() The flight data consist largely of drag measurements made by the wake-survey method. ![]() _Files_ = "AeroFoil_UI_Files/AeroFoil_Initial_Dialog.ui, AeroFoil_UI_Files/AeroFoil_NACA4Digit_Dialog.ui, \ĪeroFoil_UI_Files/AeroFoil_NACA5Digit_Dialog.ui, AeroFoil_UI_Files/AeroFoil_CurvesInput_Dialog.ui, \ĪeroFoil_UI_Files/AeroFoil_PointsInput_Dialog.ui, AeroFoil_UI_Files/AeroFoil_DATInput_Dialog.ui, \ĪeroFoil_UI_Files/AeroFoil_CSVInput_Dialog.ui, AeroFoil_UI_Files/AeroFoil_FileLoad_Dialog.ui, \ĪeroFoil_UI_Files/AeroFoil_Final_Dialog.ui, AeroFoil_UI_Files/AeroFoil_Math_Functions_Box.ui, \ĪeroFoil_UI_Files/AeroFoil_mfb_img.gif, AeroFoil_UI_Files/AeroFoil.Summary of Airfoil Data Recent airfoil data for both flight and wind-tunnel tests have been collected and correlated insofar as possible. _Help_ = "Click on the AeroFoil button/macro, and follow the instructions in the subsequent dialog boxes." _Comment_ = "AeroFoil creates airfoil curves and faces using pre-defined models, algebraic functions, and DAT or CSV Files" Absolute chord length, in millimetres, cannot be less than 1mm.Ĭaption : Preset Characters and Functions.Increasing the refine and quantity parameters increases the computation time and resources.For file imports, it is suggested to leave the line, row, and column numbers to their default values, unless you are well-informed.Curves or points that contain the bottom airfoil data cannot be mirrored.Curves or points that are intersecting between 0 and 1, both exclusive, will return an error.For curve functions, the trigonometric theta ranges from 0° to 360°, subject to computational limits.For curve functions, the trigonometric theta is in degrees ( θ °). ![]()
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