Numerical Investigation of "Transonic Resonance" With Convergent -divergent [url removed, login to view] by CFD, Fluent. First you have to draw by gambit and run in fluent.
The solution will be coupled, asixsemmetric, 2nd order, k-w, unstedy.
There must be unstedy shock at the divergent section.
You also have to post process the simulation.
The project will be similar to the allatched paper. Please the attached paper for ref
2 freelance font une offre moyenne de $250 pour ce travail
Please see our CFD profile on [url removed, login to view] We have experience in CFD simulation of Nozzle in Two CFD codes. grid independence study can also be carried out if demanded i.e. two files will be p Plus