Large-Eddy Simulation of High-Subsonic Jet Flow with Microjet Injection
Author:
Affiliation:
1. Japan Aerospace Exploration Agency (JAXA)
2. Advanced Science & Intelligence Research Institute Corporation
3. IHI Corporation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-2883
Reference29 articles.
1. On the use of microjets to suppress turbulence in a Mach 0.9 axisymmetric jet
2. The effect of streamwise vortices on the aeroacoustics of a Mach 0.9 jet
3. M. B. Alkislar, "Flow Characteristics of a Jet Controlled with Chevron-Microjet Combination for Noise Reduction", AIAA2009-851
4. S. M. Harrison etal, "Jet Noise Reduction by Fluidic Injection On a Separate Flow Exhaust System", AIAA 2007-439
5. Subsonic Jet Noise Reduction by Microjets - A Parametric Study
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