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 freelancers are bidding on average $165 for this job
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.