Advanced Technology for Aero Gas Turbine Components: Conference Proceedings Held at the Propulsion and Energetics Panel (69th) Symposium in Paris (France) on 4-8 May 1987
Abstract
The development of advanced components for new aero gas turbine propulsion systems rests on a wide range of practical and theoretical technologies. The subject was last reviewed at the 32nd PEP Meeting in 1968, and this meeting provided engineers and scientists with an opportunity to discuss recent progress in these technologies and identify requirements for further research. The scope of the meeting included: compressors, both sub- and supersonic, axial and radial; requirements and objectives for components and component integration in the complete engine; turbines, including cooling effects; combustors and afterburners, including mechanical and materials aspects; advanced propellers, and associated drive systems.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1987
- Accession Number
- ADA198664
Entities
Organizations
- AGARD