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February 4, 2019, 15:05 |
Varying Mach Number with Design Points
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#1 |
New Member
Alex
Join Date: Feb 2019
Posts: 4
Rep Power: 7 |
Hi,
I have a aerofoil modeled and meshed and I would like to vary the Mach number from 0.6 to 1.2. I have set up the boundary condtions such that the inlet velocity is a parameter and the farfield mach number is also a parameter. I would like to compute this range in small 0.5 increments and using the desing points would make easy work of this. My question is, if i change the mach number from design point to design point, do I loose my Initialization compute from and referance value. For example, In DP 1, I compute from inlet with mach=0.6, in DP 2, is the inlet Initialization still m=0.6 or is it m=0.65 as defined in the table? Thanks Al |
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February 4, 2019, 17:12 |
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#2 |
Senior Member
Lucky
Join Date: Apr 2011
Location: Orlando, FL USA
Posts: 5,764
Rep Power: 66 |
If you use "compute from" then it will use whatever properties are assigned to the boundary. So it will update to use the M=0.65.
But if you're going to vary the solution in small increments, it might be a better idea to just change the BC and not re-initialize. Just use the solution at M=0.6, change the mach number, and then keep iterating. The converged solution at M=0.6 might be a better initial condition than a blind initialization. |
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February 5, 2019, 05:10 |
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#3 |
New Member
Alex
Join Date: Feb 2019
Posts: 4
Rep Power: 7 |
Thank you for the reply LuckyTran.
Im looking to plot the Cd and Cl vs Mach number on a graph, would this be the best method of obatinign the data? I like the design points as I can export it to .cvs file. |
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ansys fluent 18.0 |
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