Surface heat transfer immediately downstream of flush, non-tangential injection holes and slots
- 9 June 1969
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Film Cooling With Injection Through Holes: Adiabatic Wall Temperatures Downstream of a Circular HoleJournal of Engineering for Power, 1968
- Heat Transfer With Film Cooling Near Nontangential Injection SlotsJournal of Engineering for Power, 1968
- 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