Complete three-dimensional multiparameter mapping of a supersonic ramp fuel injector flowfield
- 1 March 1996
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 34 (3), 455-462
- https://doi.org/10.2514/3.13089
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
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- Experimental investigation of a supersonic swept ramp injector using laser-induced iodine fluorescenceJournal of Propulsion and Power, 1994
- Investigation of a contoured wall injector for hypervelocity mixing augmentationAIAA Journal, 1993
- Vorticity generation mechanisms in parallel injection schemes for supersonic mixingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- A numerical study of mixing enhancement in a supersonic combustorPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Evaluation of parallel injector configurations for supersonic combustionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989