eb05416991
Taken from sources in CVS at:
https://sourceforge.net/projects/rocketworkbench/
Sources extracted in two steps:
1. Pull entire project tree into a subdir "rwb" via "rsync":
rsync -a a.cvs.sourceforge.net::cvsroot/rocketworkbench/ rwb/.
2. Export sources:
export CVSROOT=$(pwd)/rwb
SUBDIRS="analyser cpropep cpropep-web CVSROOT data libcompat libcpropep libnum libsimulation libthermo prop rocketworkbench rockflight"
mkdir rwbx; cd rwbx
cvs export -D now ${SUBDIRS}
After this (and some backups for safety), the directory content was
added to a Git repo:
git init .
git add *
27 lines
940 B
Plaintext
27 lines
940 B
Plaintext
This is cpropep version 1.0, a program for determining the
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theoretical performance of rocket propellant compositions.
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Cpropep is released under the GPL and is written in ANSI C.
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It has compiled successfully under the following platforms:
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. i686 Windows 98 (4.10.1998) running Microsoft Visual
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C++ 6.0 Standard Edition with Microsoft Visual Studio
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Service Pack 2
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. i686 Red Hat Linux 6.2 (Kernel 2.2.14-12) with gcc
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. i586 Debian GNU/Linux 2.2 (Kernel 2.2.16) with gcc
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To compile under linux, type make in the top-level directory.
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Under MSVC++, create a new Win32 console project file, add
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all source and header files to the project, set the header
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file directory to ..\lib\ (or copy all files from \lib to
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\cpropep or change the #include statements in cpropep.c) and
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build.
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Run using
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cpropep -h
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for command-line help and usage.
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Cpropep is Copyright (C) 2000 Antoine Lefebvre
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<antoinelefebvre@softhome.net>
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