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#1 |
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New Member
Lisa
Join Date: May 2025
Posts: 3
Rep Power: 2 ![]() |
Hi there,
I wish to plot pressure coefficient against x/chord in tecplot 360 for common research model high-lift. This plot should be for the slat, wing and flap. I took a slice which includes slat and flap but it does not look correct. Can anyone show me an example please Many thanks |
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#2 |
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New Member
gibson
Join Date: Nov 2023
Posts: 8
Rep Power: 4 ![]() |
Hi there,
It sounds like you want the pressure coefficient along the boundary of the wing, for all sections of a wing chord. This is a common goal with Tecplot 360. Here is one of our video guides doing exactly that https://tecplot.com/2022/02/25/extra...-xy-line-data/ with the Onera Wing dataset which is included with 360 installs. If you have a few more questions or find your workflow needs to be changed from this, you can reach out to Tecplot support at support@tecplot.com. Hope this helps, cheers. |
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| Tags |
| pressre distribution, tecplot360, wing surface |
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