Incompressible Center-Bore Hybrid Rocket Public

Velocity Ratio = 50

OpenFOAM simulation source files necessary to simulate the internal flow of a hybrid rocket. The attached zip file contains the directory structure which follows the normal OpenFOAM format and may be described as follows: System folder: Contains solver settings and mesh generation dictionaries Constant folder: Contains fluid and turbulence settings 0 folder: Contains boundary conditions for the steady flow problem


Items in this Work