 |
 |
 |
|
|
|
[Sponsors] | ||||
July 3, 2022, 04:52
|
Need help with PanAIr
|
#1 |
|
New Member
Join Date: Jul 2022
Posts: 1
Rep Power: 0  |
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? |
|
|
|
|
|
January 30, 2024, 03:53
|
|
#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 |
|
|
|
|
|
 |
| Tags |
| coefficient of pressure, panair, panel method |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| How to evaluate aerodynamic performance using panair? | cfda | Main CFD Forum | 0 | March 5, 2019 21:58 |
| PANAIR: PANEL METHOD CODE | Yogesh P | Main CFD Forum | 9 | October 26, 2015 18:04 |
| Help! 3d hess smith panel method | zhongyu | Main CFD Forum | 18 | December 19, 2013 13:15 |
| I am a beginner on PANAIR: Need of help! | la mimi | Main CFD Forum | 3 | February 16, 2007 21:37 |
| PanAir software | Patrick van der Velde | Main CFD Forum | 3 | April 25, 2000 10:11 |
Linear Mode
