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Enhancement of Aeroengine Combustion Chamber Air Cooling Holes Design for Emission Reduction and Pattern Factor Control
The results of a comprehensive numerical analysis of temperature uniformity and NOx and CO emission predictions in an aeroengine annular combustor liner, conducted by geometrical modifications through design changes in primary cooling air, including effusion cooling holes, are shown in the paper. A...
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| Format: | Article |
| Language: | English |
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Інститут енергетичних машин і систем ім. А. М. Підгорного Національної академії наук України
2025
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| Online Access: | https://journals.uran.ua/jme/article/view/321233 |
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