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Overview of the Hybrid Wing Body Aeroacoustic Test in NASA Langley 14- by 22- Foot Subsonic Tunnel
Document ID
20200007780
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Florence Hutcheson
(Langley Research Center Hampton, United States)
Date Acquired
May 14, 2020
Publication Date
June 16, 2014
Publication Information
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Acoustics
Report/Patent Number
Report Number: NF1676L-19172
NF1676L-19172
Meeting Information
Meeting: 20th AIAA/CEAS Aeroacoustics Conference
Location: Atlanta, GA
Country: US
Start Date: June 16, 2014
End Date: June 20, 2014
Sponsors: Council of European Aerospace Societies, American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 699959.02.07.07.08
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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