Shielding of Turbomachinery Broadband Noise from a Hybrid wing Body Aircraft Configuration
Author:
Affiliation:
1. NASA Langley Research Center
2. Northrop Grumman Corporation
3. Analytical Services and Materials, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2624
Reference16 articles.
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