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April 9, 2009, 15:27 |
Supersonic compression-ramp flow
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#1 |
New Member
Abhishek Kaushal
Join Date: Mar 2009
Posts: 2
Rep Power: 0 |
Hi everyone,
i've been trying to simulate the supersonic ciompression ramp flow on fluent. Although i was able to get the steady(mean) values of the parametes (pressure, etc) right, i'm unable to replicate intermittent pressure signal near the compression corner (shock/BL interation). till now i've tried using the spalart allmaras model only. I wonder if anyone here has ever tried it before could help me with this. thanks abhishek. |
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April 9, 2009, 16:10 |
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#2 |
New Member
sophie
Join Date: Apr 2009
Posts: 8
Rep Power: 17 |
Hi
The problem with spalart allmaras is that it is 1 equation so it have big problems to accomodate with high gradients try using density based solver (in place of pressure based) |
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April 10, 2009, 07:25 |
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#3 |
New Member
Abhishek Kaushal
Join Date: Mar 2009
Posts: 2
Rep Power: 0 |
hey sophie! thanks for replying. All this time i've been using density based SA model only. i guess RANS would do better! I'll try that now.
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June 14, 2017, 12:41 |
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#4 | |
New Member
Join Date: Oct 2016
Posts: 3
Rep Power: 10 |
Quote:
please can u help me studying this model, how you compare/validate this model please ping me on bharathikvl@gmail.com thank you |
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Tags |
boundary layer, interaction, ramp, shock, supersonic |
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