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  • Supersonic Flow Over a Wedge - Verification & Validation

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The most striking difference between the two results is the thickness of the shock. Notice that for the refined mesh, the shock is less thick that for the original mesh. This shows that the refined mesh is converging towards the real case.

Verification


Mach Number

Static Pressure

Theory Value

2.254

2.824

FLUENT Solution

2.243

2.803

Percent Difference

0.8%

0.7%

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