文件名称:PanelCode
- 所属分类：
- Linux/Unix编程
- 资源属性：
- [Windows] [Visual C] [源码]
- 上传时间：
- 2012-11-26
- 文件大小：
- 77kb
- 下载次数：
- 0次
- 提 供 者：
- X*
- 相关连接：
- 无
- 下载说明：
- 别用迅雷下载，失败请重下，重下不扣分！
介绍说明－－下载内容均来自于网络，请自行研究使用
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-scr ipt 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
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-scr ipt 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
相关搜索： panelcode
(系统自动生成,下载前可以参看下载内容)
下载文件列表
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
.............\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