PanelCode
所属分类:Windows编程
开发工具:Fortran
文件大小:77KB
下载次数:11
上传日期:2009-06-25 22:11:33
上 传 者:
XJCODE
说明: The source
code for the program is offered under the GNU General Public License.
Please feel free to download the code, read it, modify it, compile it and
run it locally.
(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
)
文件列表:
Panel Code II\common.inc (1277, 2005-02-17)
Panel Code II\Debug\DF60.PDB (33792, 2008-02-01)
Panel Code II\Debug\gaussian_elimination.obj (7627, 2005-03-16)
Panel Code II\Debug\initialize.obj (7853, 2005-03-16)
Panel Code II\Debug\inverse.obj (6525, 2005-03-16)
Panel Code II\Debug\load_coefficients.obj (10787, 2005-03-16)
Panel Code II\Debug\load_coordinates.obj (6212, 2005-03-16)
Panel Code II\Debug\load_cp.obj (7864, 2005-03-16)
Panel Code II\Debug\load_field_vars.obj (7128, 2005-03-16)
Panel Code II\Debug\load_grid.obj (17329, 2005-03-16)
Panel Code II\Debug\load_naca.obj (8735, 2005-03-16)
Panel Code II\Debug\load_streamlines.obj (9724, 2005-03-16)
Panel Code II\Debug\main.obj (4810, 2008-02-01)
Panel Code II\Debug\main.pdb (25600, 2008-02-01)
Panel Code II\Debug\makefile.obj (0, 2005-03-16)
Panel Code II\Debug\naca45.obj (3205, 2005-03-16)
Panel Code II\Debug\output.obj (4653, 2005-03-16)
Panel Code II\Debug\polynomial.obj (2984, 2005-03-16)
Panel Code II\Debug\print_cp.obj (4812, 2005-03-16)
Panel Code II\Debug\print_field_pres.obj (5166, 2005-03-16)
Panel Code II\Debug\print_foil.obj (4835, 2005-03-16)
Panel Code II\Debug\print_grid.obj (5393, 2005-03-16)
Panel Code II\Debug\print_streamlines.obj (5351, 2005-03-16)
Panel Code II\Debug\print_vectors.obj (5419, 2005-03-16)
Panel Code II\Debug\read_airfoil.obj (11353, 2005-03-16)
Panel Code II\Debug\redistribute_points.obj (3164, 2005-03-16)
Panel Code II\Debug\spline.obj (5489, 2005-03-16)
Panel Code II\Debug\splint.obj (3452, 2005-03-16)
Panel Code II\Debug\velocity.obj (6590, 2005-03-16)
Panel Code II\gaussian_elimination.f (801, 2005-02-17)
Panel Code II\initialize.f (1750, 2005-03-16)
Panel Code II\inverse.f (2085, 2005-02-17)
Panel Code II\load_coefficients.f (1917, 2005-02-17)
Panel Code II\load_coordinates.f (749, 2005-02-17)
Panel Code II\load_cp.f (1245, 2005-02-17)
Panel Code II\load_field_vars.f (609, 2005-02-17)
Panel Code II\load_grid.f (4369, 2005-02-17)
Panel Code II\load_naca.f (2858, 2005-02-17)
Panel Code II\load_streamlines.f (1522, 2005-02-17)
Panel Code II\main.dsp (3279, 2005-05-30)
... ...
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