Characterization of supersonic mixing in a nonreacting Mach 2 combustor
- 6 January 1992
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Transverse injection into Mach 2 flow behind a rearward-facing step - A 3-D, compressible flow test case for hypersonic combustor CFD validationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Mole-fraction imaging of transverse injection in a ducted supersonicflowAIAA Journal, 1991
- Low angle injection into a supersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Laser-induced iodine fluorescence technique for quantitative measurement in a nonreacting supersonic combustorAIAA Journal, 1989
- Laser methods for nonintrusive measurement of supersonic hydrogen-air combustion flowfieldsPublished by Laser Institute of America ,1988