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Temperature on the wall of an airfoil using SU2 |
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September 27, 2017, 13:53 |
Temperature on the wall of an airfoil using SU2
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#1 |
New Member
gittagawa
Join Date: Jun 2017
Posts: 24
Rep Power: 8 |
Hello,
Does anybody know how to calculate the local temperature on the wall of an airfoil using SU2? Thank you for considering my request! |
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September 27, 2017, 19:05 |
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#2 |
Member
Ole Burghardt
Join Date: Mar 2016
Location: Kiel, Germany
Posts: 60
Rep Power: 10 |
Hi there,
if you run a compressible simulation, a (gas) energy equation is a natural part of the game. If you prescribe a heatflux on the airfoil's wall - which seems to be the case - you can extract the corresponding temperature there from the flow solution file (the one SU2_SOL generates, Tecplot and Paraview ones are available). Does this answer your question? Regards, Ole |
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September 30, 2017, 11:58 |
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#3 | |
New Member
gittagawa
Join Date: Jun 2017
Posts: 24
Rep Power: 8 |
Quote:
Thank you! |
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October 1, 2017, 11:40 |
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#4 |
Member
Ole Burghardt
Join Date: Mar 2016
Location: Kiel, Germany
Posts: 60
Rep Power: 10 |
Soon it will be possible (rather think of months than years).
These kind of multi-zone problems (e.g. heat transport from a solid body into a fluid) are commonly referred to as "conjugate heat transfer". I am currently working on these but all of them involve the incompressible solver (as I am mostly concerned with liquids). However, changing the solver from the incompressible to the compressible one is just a matter of changing a few lines of code. And since the compressible side provides the much cooler test cases like turbine blades for example, I will definitely give it a try . If you PM me your mail address, I can send you an update when things are ready to use and pushed to a feature branch. Kind regards, Ole |
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