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Search: Posts Made By: Amar Fayyad
Forum: FLUENT March 8, 2016, 14:15
Replies: 3
Views: 4,141
Posted By Amar Fayyad
Hi, Since the Mach Number you deal is...

Hi,

Since the Mach Number you deal is 0.75 over a super-critical aerofoil such as VA 2, you should be considering density based solver rather than pressure based solver in order to accommodate...
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