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Supersonic Flow over a 2D Diamond Shaped Airfoil.

A Flow analysis was done on a Diamond Shaped at the 0 Degree angle of Attack with the supersonic Turbulent flow at Mach no.02. ​Pressure gradient was calculated over the airfoil 

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Software used: ANSYS Fluent

mesh_edited.jpg

01

Geometry and Meshing

02

Boundary Conditions

A steady state simulation was done using ideal gas as fluid. The flow type was Turbulent flow. K- Omega Turbulent model was used.

  • farifeild -

    • Velocity- Mach 2

    • Pressure- 50000

    • Temperature- 150K

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static pressure_edited.jpg

03

Results

Velocity Vortex- 

Streamlines- 

Project Report

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