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Search: Posts Made By: cfd seeker
Forum: FLUENT July 18, 2012, 04:54
Replies: 1
Views: 1,492
Posted By cfd seeker
Ma=0.8 is very tricky mach no. and usually...

Ma=0.8 is very tricky mach no. and usually problems arises while convergence. Due to local shocks and shock and boundary layer interaction the problem becomes very complex. After running the solution...
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