Fuels and Combustion Technology for Advanced Aircraft Engines (Les Propergols et les Systemes de Combustion pour les Moteurs d'Aeronefs)
Abstract
New technologies for low-NOx combustors and advanced high-pressure/ high-temperature cycle engines result in unique problems in design and performance. There have been significant advances in modelling and diagnostics to aid the development of these technologies. The purpose of this Symposium is to bring together experts from industry, research establishments, and universities to discuss fundamental and applied research in combustion, diagnostics, and modelling as relevant to the development of advanced gas turbine engines, to exchange practical experience, and discuss the state of the art. The Symposium focusses on high temperatures fuel systems, atomization and mixing, emissions, and combustor design and performance.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1993
- Accession Number
- ADA275679
Entities
Organizations
- AGARD