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March 29, 2020, 23:58 |
TUI coefficient of drag and lift
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#1 |
New Member
ZT
Join Date: Nov 2019
Posts: 14
Rep Power: 7 |
Morning all,
I am currently using HPC to simulate flow around a wingsuit. I have not yet found a way to find the Cl and Cd of the wingsuit, I can so far only find the lift and drag in Newtons. I am limited to using the TUI so does anybody know what the commands are to either convert the lift and drag into coefficients like you can on a Gui or just have it as coefficients in the first place? TIA, Zach |
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March 30, 2020, 05:33 |
Coefficients
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#2 |
Senior Member
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The coefficients are nothing by normalized force values. You just need to divide force in N by dynamic pressure of freestream to get coefficient values. As far as commands are concerned, you will find those under solve rep-def. But those will setup monitors. To fetch values, best would be to calculate at your end.
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Regards, Vinerm PM to be used if and only if you do not want something to be shared publicly. PM is considered to be of the least priority. |
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March 30, 2020, 08:29 |
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#3 |
New Member
ZT
Join Date: Nov 2019
Posts: 14
Rep Power: 7 |
Hi there,
Thanks for your answer. I can get cd and cl when I set them up on the GUI, should there not be some TUI system for doing this as well? It seems counterintuitive. |
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March 30, 2020, 09:40 |
GUI and TUI
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#4 |
Senior Member
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Not every command in TUI has a parallel option in GUI, similarly, not every GUI option has a TUI command. You can setup a monitor for coefficient, you can print their values as the simulation proceeds, but there is no option to compute by giving a command. Possibly in future release.
__________________
Regards, Vinerm PM to be used if and only if you do not want something to be shared publicly. PM is considered to be of the least priority. |
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Tags |
coefficients, tui |
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