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July 5, 2020, 11:36 |
Mach 2 flow over cavity.
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#1 |
New Member
Harjit
Join Date: Feb 2020
Posts: 7
Rep Power: 6 |
Hi everyone,
I'm currently trying to simulate flow at Mach 2 over a cavity. For the inlet I've used the steady state solution for a flat plate since in this way the boundary layer is already formed. The outlet and upper wall are set on pressure-far-field with the free stream conditions specified. The density is set as ideal-gas and the free stream conditions are: M_inf=1.5 P_inf=66.4 kPa T_inf=218 K. I have used the interpolation for initializing the transient problem. However, the results I've obtained do not make any sense. I have attached the figures. I've also tried to extend the inlet wall and putting the inlet as pressure-far-field and it didn't work. How can I fix it? Thanks in advance. Last edited by harji95; July 5, 2020 at 11:50. Reason: Wrong post |
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