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#1 |
New Member
Join Date: Jul 2022
Posts: 1
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I ran multiple models (supersonic and subsonic) in PanAir to verify the results from published papers. I am getting Varied Coefficient of Pressure than that of the papers.
Procedure I use: 1.Create a model in catia. 2.Create planes and points on the model. 3.Extract the points. convert them to a .wgs format. 4.Create an auxilliary file for Panin convertor to get an input file to run in Panair. What am I doing wrong? |
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#2 |
New Member
Tosbaga
Join Date: Mar 2017
Location: Earth
Posts: 19
Rep Power: 9 ![]() |
Buddy, I've looked at your file, you are missing the wake panels for the wing. Without wake panels the solution you are getting is not physical.
Regards Last edited by Tosbaga; January 30, 2024 at 03:54. Reason: typo |
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Tags |
coefficient of pressure, panair, panel method |
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