Experimental investigation of a supersonic shear layer with slot injection of helium
- 1 September 1991
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 29 (9) , 1426-1435
- https://doi.org/10.2514/3.10756
Abstract
No abstract availableThis publication has 19 references indexed in Scilit:
- Low angle injection into a supersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Liquid fueled supersonic combustion ramjets - A research perspectiveof the past, present and futurePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Skin Friction Reduction by Injection Through Combinations of Slots and Porous SectionsAIAA Journal, 1975
- Experimental Study of Slot Injection into a Supersonic StreamAIAA Journal, 1973
- Film cooling effectiveness in hypersonic turbulent flowAIAA Journal, 1970
- The influence of foreign gas injection and slot geometry on film cooling effectivenessInternational Journal of Heat and Mass Transfer, 1969
- Supersonic transverse injection into a supersonic stream.AIAA Journal, 1968
- On the use of a boundary-layer model for correlating film cooling dataInternational Journal of Heat and Mass Transfer, 1967
- Film cooling with helium injection into an incompressible air flowInternational Journal of Heat and Mass Transfer, 1966
- Film cooling with air and helium injection through a rearward-facingslot into a supersonic air flow.AIAA Journal, 1966