w12sc3 (1)
所属分类:数学计算
开发工具:Fortran
文件大小:251KB
下载次数:1
上传日期:2019-04-28 01:58:04
上 传 者:
sbeetlebum
说明: Combines source and vortex panel singularities for calculating the linear theory estimate of supersonic configuration aerodynamics.
文件列表:
case1.inp (6670, 2005-12-01)
case1.out (141448, 2005-11-10)
files.cmn (333, 2005-11-30)
head.cmn (139, 2005-11-10)
input.txt (146, 2005-12-20)
lar13239.txt (2917, 2005-12-20)
option.cmn (210, 2005-11-10)
shell.cmn (328, 2005-12-01)
w12sc3.f90 (450136, 2008-11-11)
original.src (1227849, 2010-11-29)
W12SC3- SUPERSONIC WING DESIGN AND ANALYSIS \w12sc3\readme.txt
The files for this program are in the directory \w12sc3 on the CD-ROM and in the
archive file w12sc3.zip that may be downloaded from the PDAS web site.
readme.txt this file of general description
input.txt guide to preparing input file
w12sc3.f90 the complete source code
files.cmn description of common block /FILES/
head.cmn description of common block /HEAD/
option.cmn description of common block /OPTION/
shell.cmn description of common block /SHELL/
lar13239.txt the original program description from COSMIC
original.src the original copy of the source code (from COSMIC)
Sample cases for this program are:
case1.inp input data
case1.out output data for case1.inp
To compile this program for your computer, use the command
gfortran w12sc3.f90 -o w12sc3.exe
Linux and Macintosh users may prefer to omit the .exe on the file name.
This program first asks for the name of the input file. This must
be a file written to conform to input.txt. After calculating
the solution, the program produces a file called w12sc3.out that contains
a wealth of information concerning the flow problem to be solved.
There still may be problems with this code. I have only been
checking it for a short time, but I thought it would be OK to go
ahead and release it.
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