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  • Supersonic Flow Over a Wedge - Verification & Validation

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Old Version 39

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New Version 40

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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

Theory Value

2.254

FLUENT Solution

2.243

Percent Difference

0.8%

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