Evaluation of heat transfer for film-cooled turbine components
Authors:
- 1 January 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 8 (1) , 33-38
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Film Cooling of an Adiabatic Flat Plate in Zero Pressure Gradient in the Presence of a Hot Mainstream and Cold Tangential Secondary InjectionJournal of Heat Transfer, 1965
- A note on the use of a boundary-layer model for correlating film-cooling dataInternational Journal of Heat and Mass Transfer, 1965
- Velocity Distributions, Temperature Distributions, Effectiveness and Heat Transfer for Air Injected Through a Tangential Slot Into a Turbulent Boundary LayerJournal of Heat Transfer, 1961
- Heat Transfer and Effectiveness for a Turbulent Boundary Layer With Tangential Fluid InjectionJournal of Heat Transfer, 1960