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[ICEM] How to improve the mesh of 3D highly twisted axial compressor blade

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Old   April 18, 2018, 13:12
Default How to improve the mesh of 3D highly twisted axial compressor blade
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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?
Attached Images
File Type: jpg block-edited.jpg (164.0 KB, 13 views)
File Type: jpg blocking_edited.jpg (151.3 KB, 13 views)
File Type: jpg block-tip-edited.jpg (49.8 KB, 14 views)
File Type: jpg flow-edited.jpg (58.1 KB, 13 views)
File Type: jpg mesh-tip-edited.jpg (70.2 KB, 16 views)
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Old   April 18, 2018, 13:13
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more photos
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Old   April 18, 2018, 13:16
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Here shows the bad elements (sharp -edged)
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Old   April 18, 2018, 18:08
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Why don't you smooth your mesh? Try Laplacian method, and quality will improve significantly.
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