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PanelCode

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  • Update : 2012-11-26
  • Size : 77kb
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Introduction - If you have any usage issues, please Google them yourself
Parameter definitions: use_naca: logical, true if we want to generate a NACA 4/5 digit airfoil internally, false if we should read the coordinates from the UIUC database. naca: integer NACA 4/5 digit number. Note, no error checking is performed here to see if it s a valid number. that s done by the perl-script that executes this code, so make sure you give it a valid number. airfoil: string, name of the database airfoil to read, including the relative path-name. smoothing: logical, true if you want to smooth the surface points that you read from a file. Note, smoothing will alter the airfoil data, however, unsmoothed data may result in ripples in the pressure. npanels: integer number of panels for the simulations. If you want to use more than 200, increase the value of ndim in the common.inc file
Packet file list
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Panel Code II
.............\common.inc
.............\Debug
.............\.....\DF60.PDB
.............\.....\gaussian_elimination.obj
.............\.....\initialize.obj
.............\.....\inverse.obj
.............\.....\load_coefficients.obj
.............\.....\load_coordinates.obj
.............\.....\load_cp.obj
.............\.....\load_field_vars.obj
.............\.....\load_grid.obj
.............\.....\load_naca.obj
.............\.....\load_streamlines.obj
.............\.....\main.obj
.............\.....\main.pdb
.............\.....\makefile.obj
.............\.....\naca45.obj
.............\.....\output.obj
.............\.....\polynomial.obj
.............\.....\print_cp.obj
.............\.....\print_field_pres.obj
.............\.....\print_foil.obj
.............\.....\print_grid.obj
.............\.....\print_streamlines.obj
.............\.....\print_vectors.obj
.............\.....\read_airfoil.obj
.............\.....\redistribute_points.obj
.............\.....\spline.obj
.............\.....\splint.obj
.............\.....\velocity.obj
.............\gaussian_elimination.f
.............\initialize.f
.............\inverse.f
.............\load_coefficients.f
.............\load_coordinates.f
.............\load_cp.f
.............\load_field_vars.f
.............\load_grid.f
.............\load_naca.f
.............\load_streamlines.f
.............\main.dsp
.............\main.dsw
.............\main.f
.............\main.ncb
.............\main.opt
.............\main.plg
.............\makefile.f
.............\naca45.f
.............\output.f
.............\polynomial.f
.............\print_cp.f
.............\print_field_pres.f
.............\print_foil.f
.............\print_grid.f
.............\print_streamlines.f
.............\print_vectors.f
.............\read_airfoil.f
.............\redistribute_points.f
.............\spline.f
.............\splint.f
.............\velocity.f
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