Investigation of multiple slot film cooling to a blunt nose cone
- 16 July 1973
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Film-Cooling Effectiveness and Skin Friction in Hypersonic Turbulent FlowAIAA Journal, 1972
- An experimental investigation of turbulent slot injection at Mach 6AIAA Journal, 1970
- A note on the use of a boundary-layer model for correlating film-cooling dataInternational Journal of Heat and Mass Transfer, 1965
- Laminar, Transitional and Turbulent Heat Transfer to a Cone-Cylinder-Flare Body at Mach 8.0Journal of the Aerospace Sciences, 1962
- Helium Injection Into the Boundary Layer at an Axisymmetric Stagnation PointJournal of the Aerospace Sciences, 1962
- Velocity Distributions, Temperature Distributions, Effectiveness and Heat Transfer for Air Injected Through a Tangential Slot Into a Turbulent Boundary LayerJournal of Heat Transfer, 1961
- Film Cooling With Multiple Slots and LouversJournal of Heat Transfer, 1961
- Heat Transfer and Effectiveness for a Turbulent Boundary Layer With Tangential Fluid InjectionJournal of Heat Transfer, 1960