Direct measurements at Mach 6 of turbulent skin-friction reduction by injection from single and multiple flush slots
- 26 January 1976
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Investigation of the three-dimensional turbulent flow downstream of swept slot injection in hypersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Investigation of multiple slot film cooling to a blunt nose conePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Film-Cooling Effectiveness and Skin Friction in Hypersonic Turbulent FlowAIAA Journal, 1972
- Multiple slot laminar film coolingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Film CoolingPublished by Elsevier ,1971
- The drag of a compressible turbulent boundary layer on a smooth flat plate with and without heat transferJournal of Fluid Mechanics, 1964
- GASEOUS FILM COOLING WITH MULTIPLE INJECTION STATIONSAIAA Journal, 1963