An analytical investigation of angled injection into a compressible flow
- 1 July 1996
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Experimental investigation of angled injection in a compressible flowJournal of Propulsion and Power, 1996
- The use of swirling jet pairs to provide rapid fuel penetration in scramjet combustorsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Computational/experimental investigation of staged injection into a Mach 2 flowAIAA Journal, 1994
- Three-dimensional computations of cross-flow injection and combustion in a supersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Analytic and approximate boundary-fitted coordinate systems for fluid flow simulationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980