I will do supersonic nozzle cfd simulation using ansys fluent

Hi, I'm Laiba. I am an aerospace engineering student with hands-on experience in supersonic nozzle CFD using ANSYS Fluent.

I will perform CFD simulation for your convergent-divergent nozzle. This is useful for rocket engines, jet propulsion, wind tunnels, and industrial gas flow.

What I deliver:

- 2D or 3D CFD simulation

- Mach number contours to check supersonic flow

- Static pressure and temperature distribution

- Velocity contours and streamlines

- Shock wave detection

- Quality mesh with inflation layers

- Short report explaining results

My experience:

I am working on a variable petal-based nozzle for my final year project. I have also completed multiple nozzle simulations using ANSYS Fluent and NASA CEA.

What I need from you:

- Nozzle geometry (STEP, IGES, or dimensions)

- Inlet pressure and temperature

- Back pressure (ambient condition)

- Gas type (air, nitrogen, etc.)

If you don't have a geometry file, I can create a basic CD nozzle from your area ratio.

Message me before ordering if you have questions. I respond within a few hours.

Thank you.