Actions: CombustionToolbox/combustion_toolbox
Actions
Showing runs from all workflows
196 workflow runs
196 workflow runs
ROCKET problem without defining an exit area ratio (subsonic or supersonic region) #1044
CI
#746:
Pull request #1045
opened
by
AlbertoCuadra
computeThermodynamics method and error in equilibrateT for thermally perfect gases, and rewrite example using OOP version
CI
#745:
Pull request #1043
opened
by
AlbertoCuadra