Noise Scattering by the Blended Wing Body Airplane: Measurements and Prediction
Author:
Affiliation:
1. North Carolina State University
2. NCI Information Systems, Inc.
3. National Institute of Aerospace
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-2474
Reference14 articles.
1. Agarwal, A. and Dowling, A. P."TheCalculation ofAcousticShieldingofEngineNoisebytheSilent Aircraft Airframe," AIAA Paper 2005-2996,May2005.
2. Hill, G. A., Brown, S. A., Geiselhart, K. A. and Burg, C. M. "Integration of Propulsion-Airframe-Aeroacoustic Technologies and Design Concepts for aQuiet Blended-Wing-BodyTransport,"AIAA Paper2004-6403, September 2004.
3. Clark, L. R., and Gerhold, C. H. "Inlet Noise Reduction by Shielding for the Blended-Wing-Body Airplane," AIAA paper 99-1937,May1999.
4. Gerhold, C. H., Dunn, M. H., Clark, L. R. and Tweed, J. "Investigation of Acoustical Shielding by a Wedge-Shaped Airframe,"AIAA Paper2004-2866, May2004.
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