[Rocketworkbench-devel] cpropep

[Antoine L. <an...@st...>]

Hello,

I finally decide to implement the theory of the book from the nasa,
Computer program for calculation of complex chemical
equilibrium compositions, rocket performance, incident and
reflected shocks, and Chapman-Jouguet detonations   

I implement the matrix to solve problem with fixed temperature and pressure. I don't see however how to compute the new mixture approximation from the Lagrange multiplier and other parameter. If someone here have an idea, I would like to know. 

There is the complete source code in the book but I have problem to understand the fortran and don't see how they do.

I wait your comments

-- 
Antoine Lefebvre
ant...@po...