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aerospike simulation at mach number 6 using Fluent 6.3
Dear All..
I am trying to do a hypersonic flow simulation over a spiked blunt body at mach 6 using fluent 6.3 In my case, I use first order upwind scheme and get a very well converged solution. however, when I switch to second order upwind scheme, totally diverge Any one has some suggestion to resolve this problem? |
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