This Repository contains everything needed to complete a basic CFD analysis of a Rocket Nozzle cross section. The analysis will be performed using the basic specifications from a SpaceX Merlin 1D engine
The repository contains the following basic sections:
- Pre-processing:
- Matlab Code to generate it (a lightly modified version of: https://github.com/Vinayak-D/MOC-MATLAB)
- Surface Generated in SolidWorks
- Fluent Mesh file
- OpenFoam Simulation:
- Files needed to execute the simulation using the rhoCentralFoam solver in OpenFoam
- list of intructions
- Post-processing
- contour plots, volume animations, force plot, etc...
Please let me know if you have any questions