Fluidic Injection on a Supersonic Jet at Various Mach Numbers
Author:
Affiliation:
1. Aerospace Engineering, University of Cincinnati, Cincinnati, Ohio 45221
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J010000
Reference45 articles.
1. Evolution from ‘Tabs’ to ‘Chevron Technology’ - A Review
2. Turbulence Measurements of Separate Flow Nozzles with Mixing Enhancement Features
3. Mean Flow and Noise Prediction for a Separate Flow Jet with Chevron Mixers
4. Flow field characterization of coaxial conical and serrated (chevron) nozzles
5. Understanding How Chevrons Modify Noise in Supersonic Jet with Flight Effects
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