Inlet noise reduction by shielding for the blended-wing-body airplane-Reference-Cited by-同舟云学术

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Inlet noise reduction by shielding for the blended-wing-body airplane

Published:1999-05-10 Issue: Volume: Page:
ISSN:
Container-title:5th AIAA/CEAS Aeroacoustics Conference and Exhibit
language:
Short-container-title:

Author:

Clark Lorenzo¹,Gerhold Carl¹

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-1937

Reference11 articles.

1. The Boeing Company, Long Beach, CA, "Blended-Wing-Body Technology Study," Final Report No. CR AD-9405TR-3780, prepared for NASA-Langley ResearchCenter underNASl-20275, October1997.

2. Hubbard, Harvey H.; and Manning, James C. "Aeroacoustic ResearchFacilities at NASA Langley ResearchCenter,"NASA TM 84585,March 1983.

3. Table 1. Configurations tested(only centerengine

4. nacelle is represented) Conflguratlon

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1. The U.S. Air Force Next-Generation Air-Refueling System: A Resurgence of the Blended Wing Body?;Aerospace;2024-06-20

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3. Boundary element analysis on the fuselage scattering of drone noise;International Journal of Aeroacoustics;2022-02-26

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