Computational-Fluid-Dynamics (CFD)

CFD Solver for Laval Nozzle and Shock Tube (one-dimensional Riemann problem)

This project is based on the mathematical fundamentals of the CFD course conducted by the institute of Thermal Turbomachinery and Machine Dynamics at Graz University of Technology. Course Link

Implemented 1D CFD Solvers C++

• Central
• LaxWendroff
• MacCormack
• ROE

UserInterface in C#/.NET WPF

The C++ CFD solver is wrapped and provides data via a C++/CLI interface to the UI. --> C++/CLI extension of Visual Studio must be installed to compile this project.

Exercise 1 Laval Nozzle

Exercise 2 Shock Tube

License

MIT