Enhancement of mixing in high-speed heated jets using a counterflowing nozzle
- 1 November 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 31 (11), 2033-2038
- https://doi.org/10.2514/3.11887
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Mixing enhancement due to global oscillations in jets with annular counterflowAIAA Journal, 1993
- The influence of velocity and density ratio on the dynamics of spatially developing mixing layersPhysics of Fluids A: Fluid Dynamics, 1992
- The stability of countercurrent mixing layers in circular jetsJournal of Fluid Mechanics, 1991
- The absolute-convective transition in subsonic mixing layersPhysics of Fluids A: Fluid Dynamics, 1989
- Initial turbulence effect on jet evolution with and without tonal excitationPhysics of Fluids A: Fluid Dynamics, 1989
- Effects of nozzle exit boundary-layer conditions on excitability of heated free jetsAIAA Journal, 1989
- Absolute instability in hot jetsAIAA Journal, 1988
- Saturation and the limit of jet mixing enhancement by single frequency plane wave excitation - Experiment and theoryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Centerline Mach number characteristics of highly heated free jetsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Effects of the initial condition on the axisymmetric free shear layer: Effects of the initial momentum thicknessPhysics of Fluids, 1978