Heat Transfer and Cooling in Gas Turbines (Le Transfert Thermique et le Refroidissement dans les Turbines a Gaz)
Abstract
The Conference Proceedings contains the 38 papers presented at the Propulsion and Energetics Panel 80th Symposium on Heat Transfer and Cooling in Gas Turbines which was held from 12th-16th October 1992 in Antalya, Turkey. The Technical Evaluation Report and the Keynote Address are included at the beginning, and discussions follow most papers. The Symposium was arranged in the following Sessions: Turbine Blades: External Heat Transfer; Turbine Blades: Internal Heat Transfer; Measurement Techniques; Rotating Disks, Labyrinth Seals and Shafts; Combustors; Design, Interactions; and Prediction Methods. Heat transfer and cooling in gas turbines are still key factors for achieving high performance, increased life and improved rehability. Any progress in this field will lead to a reduction of maintenance cost and fuel consumption. The purpose of the Symposium was to bring together experts from industry, research establishments and universities to discuss fundamental and applied heat transfer problems relevant to gas turbines, to exchange practical experience gained and to review the state of the art.
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 01, 1993
- Accession Number
- ADA264177
Entities
Organizations
- AGARD