Jet Noise Shielding for Advanced Hybrid Wing-Body Configuration
Author:
Affiliation:
1. University of California, Irvine
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-912
Reference17 articles.
1. Design of the Blended Wing Body Subsonic Transport
2. Von Glahn, U., Groesbeck, D., and Reshotko, M. "Geometry Considerations for Jet Noise Shielding with CTOL Engine-Over-The-Wing Concept,"AIAAPaper74-568, June1974.
3. Von Glahn, U., Groesbeck, D., and Wagner, J. "Wing Shielding of High-Velocity Jet and Shock-AssociatedNoise with Cold and Hot FlowJets," AIAAPaper76-547,July1976.
4. Papamoschou, D., and Mayoral, S. "Experiments on Shielding of Jet Noise by Airframe Surfaces," AIAA Paper2009-3326,May2009.
5. Mayoral, S., and Papamoschou, D. "Effects of Source Redistribution on Jet Noise Shielding," AIAA Paper 2010-0652, Jan.2010.
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