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September 26, 2014, 08:10 |
anomalous mach number
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#1 |
Member
wangjian
Join Date: Nov 2013
Posts: 54
Rep Power: 13 |
I simulate a hypersonic aircraft. The mach number of farfield is 6.0. But when the residual of density reaches -7, the resulting highest mach number reaches 1200. I use the eluer solver, and the quality of mesh is good. I want to know the reason of the situation. Can you help me?
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October 20, 2014, 15:34 |
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#2 | |
Senior Member
Heather Kline
Join Date: Jun 2013
Posts: 309
Rep Power: 14 |
Quote:
Can you please post some more information, like Reynolds number and your other boundary conditions? The residual magnitude of 10^-7 does not necessarily indicate convergence - how much was the residual reduced from initial values? Have you tried looking at the history of the residual to see if it might be diverging? |
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October 21, 2014, 05:32 |
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#3 | |
Member
wangjian
Join Date: Nov 2013
Posts: 54
Rep Power: 13 |
Quote:
Thank you very much. |
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October 24, 2014, 00:17 |
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#4 | |
Senior Member
Heather Kline
Join Date: Jun 2013
Posts: 309
Rep Power: 14 |
Quote:
You may want to try moving the "outlet" boundary further away from the vehicle and change it to a farfield condition. Currently you have a situation where at the boundary between "outlet" and "farfield" you have discontinuous conditions. This is also imposing a pressure very close to the back of your vehicle. I can't really see the geometry clearly in your picture, but you may also want to check whether the angle at the back of your vehicle exceeds the maximum Prandtl-Meyer turning angle. |
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October 24, 2014, 01:26 |
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#5 |
Member
wangjian
Join Date: Nov 2013
Posts: 54
Rep Power: 13 |
OK, I will try. Thank you.
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