Effect of film cooling/regenerative cooling on scramjet engine performances
- 1 September 1994
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 10 (5) , 618-624
- https://doi.org/10.2514/3.23771
Abstract
No abstract availableThis publication has 18 references indexed in Scilit:
- Experimental investigation of a supersonic shear layer with slot injection of heliumAIAA Journal, 1991
- Parametric study of airframe-integrated scramjet cooling requirementJournal of Propulsion and Power, 1991
- Supersonic film coolingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Experimental studies of shock wave/wall jet interaction in hypersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Experimental results for film cooling in 2-D supersonic flow including coolant delivery pressure, geometry, and incident shock effectsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Skin Friction Reduction by Injection Through Combinations of Slots and Porous SectionsAIAA Journal, 1975
- An experimental investigation of turbulent slot injection at Mach 6AIAA Journal, 1970
- Film cooling with air and helium injection through a rearward-facingslot into a supersonic air flow.AIAA Journal, 1966
- 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