Elegant Concept for Reduction of Jet Noise from Turbofan Engines
Author:
Affiliation:
1. The Boeing Company, Seattle, Washington 98124
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.11432
Reference7 articles.
1. Nozzle Shaping for Reduction of Jet Noise from Single Jets
2. Effect of excitation on coaxial jet noise
3. Parametric study of noise from dual-stream nozzles
4. Noise of Dual-Stream Beveled Nozzles at Supercritical Pressure Ratios
5. Jet Aeroacoustic Testing: Issues and Implications
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