Hello
I have upload an html version of the documentation I begin to write. The url is http://rocketworkbench.sourceforge.net/cpropep/index.html
I would appreciate any comments about that. There is probably a lot of english mistake, my native language is french...
If some more explanation are needed, please ask and I will add it.
Cpropep is now able to compute adiabatic flame temperature for some mix. As an example, cpropep predict a temperature of 1733 K for the KNO3/Sucrose propellant while propep say 1755.
I will try to install a new cgi script during the next week to let you experiment with that.
--
Antoine Lefebvre
ant...@po...
|