Compression Corner ( Hypersonic Flow ) -- CFD Online Discussion Forums

March 10, 2015, 16:59

Compression Corner ( Hypersonic Flow )

Redoctober

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Join Date: Jun 2014

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Dear FOAMers,

I am currently working on a Hypersonic simulation for a project. I am stuck with some oscillating shockwave. It is supposed to be a steady oblique shock.

The flow is,

M = 7
Cp is according to Janaf Table
Inviscid flow.

The solver being used is rhoCentralFoam

The compression corner is 30 degrees.

Any advice or help regarding how to fix this issue is appreciated ..

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