Turbine Aerothermal Research
Abstract
This in-house task was funded under AFOSR ILIR grants 92PR07COR and 02PR02COR. This task and its predecessors have been in continual operation since 1985 and have covered a broad range of topics relating to the aerodynamics and thermodynamics of the turbine module of gas turbine engines. The work initially focused on the effects of very high turbulence freestream flows on the development of the boundary layers of the turbine component, with particular attention to the effect on heat transfer. It has also pursued techniques for the control of airfoil boundary layers and cooling flows and the development of advanced techniques for the measurement and study of these flows.
Document Details
- Document Type
- Technical Report
- Publication Date
- May 01, 2012
- Accession Number
- ADA565847
Entities
People
- Richard Rivir
- Rolf Sondergaard
- Shichuan Ou
Organizations
- Air Force Research Laboratory