I want to simulate convergent divergent (CD) nozzle by fluent. First you have to draw the CD nozzle by gambit (drawing is shown in the attached file). Then simulate in Fluent (coupled, 2D, unsteady, asixsymmetric, 2nd order). There will be a unsteady lambda shock in the diverging section.
For anyother details please see the attatched file.
5 freelance ont fait une offre moyenne de 165 $ pour ce travail
Hi, I have a Masters in CFD and I am an expert in many CFD codes. My specialty is in Aerospace Engineering. I am sure I can do the project. Please see the PM.