Description: 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
- [NACA] - calculated NACA4- airfoil procedures, th
- [aerofoil] - one can generally drawings (CAD or other
- [inviscid_eqution] - Solution of viscous Burger equation and
- [EulerCode] - ROUTINES FOR GENERATION OF A C-TYPE GRID
File list (Check if you may need any files):
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
Download