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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Bibliographic Details
Main Author: Masoud Hajivand
Format: Article
Language:English
Published: NAS of Ukraine, A. Pidhornyi Institute of Mechanical Engineering Problems 2024-12-01
Series:Journal of Mechanical Engineering
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