Mean Flow Development in Dual-Stream Compressible Jets
Author:
Affiliation:
1. University of California, Irvine, Irvine, California 92697-3975
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1762
Reference25 articles.
1. On the noise sources of the unsuppressed high-speed jet
2. Mach Wave Elimination in Supersonic Jets
3. Noise Measurements in Supersonic Jets Treated with the Mach Wave Elimination Method
4. Directional Suppression of Noise from a High-Speed Jet
5. ‘Crackle’: an annoying component of jet noise
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