Aerospace, Volume 11, Issue 1
2024 January - 101 articles
Cover Story: A chemical reactor network model is proposed to simulate aeroengine burner emission and efficiency performance. In contrast to similar methods, its simplified partitioning into three subvolumes according to the axial distribution of the different air streams, paired with a proposed empirical tuning method, promotes the generality of the model without requiring engine-specific data. Its configuration produces a robust model capable of employing detailed kerosene combustion schemes to compute design-sensitive predictions of NOx, CO and unburnt hydrocarbons emissions. The model’s prediction trends are validated over actual engine tests and correlation methods, and it is integrated into open and closed design optimization loops to enhance the combustor’s performance. View this paper - Issues are regarded as officially published after their release is announced to the table of contents alert mailing list .
- You may sign up for email alerts to receive table of contents of newly released issues.
- PDF is the official format for papers published in both, html and pdf forms. To view the papers in pdf format, click on the "PDF Full-text" link, and use the free Adobe Reader to open them.