Mixing enhancement by and noise characteristics of streamwise vortices in air jet
- 1 March 1994
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 32 (3), 464-471
- https://doi.org/10.2514/3.12009
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- Manipulation of free shear flows using piezoelectric actuatorsJournal of Fluid Mechanics, 1993
- Supersonic jet mixing enhancement by 'delta-tabs'Published by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Supersonic jet mixing enhancement by vortex generatorsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Shear flow control by mechanical tabsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Vortex induction and mass entrainment in a small-aspect-ratio elliptic jetJournal of Fluid Mechanics, 1987
- Bifurcation of round air jets by dual-mode acoustic excitationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Passive control of jets with indeterminate originsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- The distortion of a jet by tabsJournal of Fluid Mechanics, 1975
- Evaluation of Hypermixing for Thrust Augmenting EjectorsJournal of Aircraft, 1974
- An experimental investigation of the composition of jet noiseJournal of Fluid Mechanics, 1969