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[ICEM] How to improve the mesh of 3D highly twisted axial compressor blade |
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April 18, 2018, 13:12 |
How to improve the mesh of 3D highly twisted axial compressor blade
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#1 |
Member
Join Date: Aug 2011
Posts: 33
Rep Power: 15 |
Hello,
I am trying to do a 3D mesh of a single axial compressor blade, which is highly twisted and tapered from hub to tip. However, I am not satisfied with the quality of the mesh and need your suggestion on how to improve it. 1. One thing to note is that the blade is having a large (negative) angle of attack (assuming the air is flowing from left to right, horizontally) >>> from my current meshing strategy, gives me sharp-edged elements around the leading and trailing edges. What would be a better strategy to avoid such sharp elements? 2. I managed to get a nicely mapped mesh around the blade surfaces, however, the internal elements are of low quality, especially around the leading and trailing edge. How can I improve this? |
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April 18, 2018, 13:13 |
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#2 |
Member
Join Date: Aug 2011
Posts: 33
Rep Power: 15 |
more photos
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April 18, 2018, 13:16 |
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#3 |
Member
Join Date: Aug 2011
Posts: 33
Rep Power: 15 |
Here shows the bad elements (sharp -edged)
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April 18, 2018, 18:08 |
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#4 |
Senior Member
Gert-Jan
Join Date: Oct 2012
Location: Europe
Posts: 1,928
Rep Power: 28 |
Why don't you smooth your mesh? Try Laplacian method, and quality will improve significantly.
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