Mixing enhancement of compressible jets by using unsteady microjets as actuators

AIAA Journal

Volumn 40, Issue 4, 2002, Pages 681-688

  Ibrahim, Mohammed K ^a   Kunimura, Ryoji ^a   Nakamura, Yoshiaki ^a  

^a NAGOYA UNIVERSITY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; COMPRESSIBLE FLOW; FLOW CONTROL; NOZZLES; SHEAR FLOW; STABILITY; UNSTEADY FLOW;

COMPRESSIBLE JETS; MICROJETS;

JETS;

EID: 0036530369     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1700     Document Type: Article

References (21)

1. Jet mixing enhancement by high-amplitude fluidic actuation
2. Control of an axisymmetric jet using vortex generator
3. Control of jet structure by crown-shaped nozzles
4. Spreading characteristics of compressible jets from nozzle of various geometrics
5. Using controlled unsteady fluid mass addition to enhance jet mixing
6. Variable control of jet decay
7. Vectoring and small-scale motions effected in free shear flows using synthetic jet actuators
8. Active flow control technology transition: The boeing ACE program
9. Numerical simulation of compressible synthetic jet flows
10. Acoustic sources in a turbulent jet: A direct numerical simulation study
11. The effects of pulsed blowing on jet mixing and noise generation
12. Measurement of mean static pressure and far-field acoustics of shock containing supersonic jets
13. Miniture fluidic oscillators for flow and noise control
14. Experiments on the flow and acoustic properties of a moderate-reynolds-number supersonic jet
15. Effects of counterflow on the aeroacoustic properties of supersonic jet
16. Survey on jet instability theory
17. Discrete acoustic radiation generated by jet instability
18. The spatial viscous instability of axisymmetric jets
19. Stability of slowly diverging jet flow
20. Helical instabilities of slowly diverging jets