Aeroacoustics of Twin Rectangular Jets Including Screech: Large-Eddy Simulations with Experimental Validation
Author:
Affiliation:
1. Stanford University, Stanford, California 94305
2. University of Cincinnati, Cincinnati, Ohio 45221
Funder
Office of Naval Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060895
Reference67 articles.
1. Aeroacoustic Experiments with Twin Jets
2. BozakR.WernetM. P. “Subsonic Round and Rectangular Twin Jet Flow Effects,” AIAA Paper 2014-3736, 2014. 10.2514/6.2014-3736
3. BridgesJ. E.BrownC. A.BozakR. “Experiments on Exhaust Noise of Compressible Fluids,” AIAA Paper 2014-2904, 2014. 10.2514/6.2014-2904
4. Exploring Physics and Control of Twin Supersonic Circular Jets
5. Aeroacoustics of Twin Supersonic Jets: A Review
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