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[ANSYS Meshing] High Mesh Skewness on Cusp Trailing Edge |
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January 28, 2018, 01:07 |
High Mesh Skewness on Cusp Trailing Edge
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#1 |
New Member
Joel
Join Date: Jan 2018
Posts: 1
Rep Power: 0 |
Hey everyone, I've been running a quasi-2D analysis on an airfoil in CFX and for some reason I keep getting minor fluctuations in lift, drag, and moment coefficients every time a run a simulation. I think its because of the high skewness in my mesh at the cusp trailing edge. I attached a photo of the inflation layers in that area. Any idea how I can go about fixing it?
Thanks a lot! |
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September 2, 2021, 03:12 |
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#2 |
New Member
Aideal Zohary
Join Date: Feb 2019
Location: Malaysia
Posts: 28
Rep Power: 7 |
Hi, this is an old thread. But if anyone is still interested to run a simulation on the NACA 0012, NACA 4415, FX 61-184 E420 and S1223 airfoil, please take a look at:
Numerical Investigation on the Pressure Drag of Some Low-Speed Airfoils for UAV Application. https://doi.org/10.37934/cfdl.13.2.2948 Unsteady 3-equation k omega intermittency SST was used. Good comparison with XFOIL and experimental data. Transition features also shown through cf and cp plots. Learn how I designed the mesh here: https://www.youtube.com/watch?v=qZRqBu9Ss2U |
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September 5, 2021, 16:12 |
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#3 |
New Member
Ali
Join Date: Aug 2021
Posts: 4
Rep Power: 5 |
hi jmcquaid
Check the following document. it is a very good resource for ansys meshing https://drahmednagib.com/CAD_2018/Le..._Meshing_2.pdf i hope it helps |
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