Computational Fluid Dynamics of Converging-Diverging Rocket Nozzles

This project was done as part of Prof. Dilip Sundaram's CFD course at IITGn. The problem statement involved predicting the fluid flow through a converging-diverging nozzle. A program was developed to solve unsteady, inviscid, compressible fluid flow through a C-D nozzle using an explicit, time-marching MacCormack scheme, and the results were validated against analytical and NASA experimental data.