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Hybrid Wing Body Acoustic Test in the 14 by 22 ft Subsonic Tunnel
Document ID
20200004720
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Thomas Brooks
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
May 11, 2020
Publication Date
October 21, 2010
Subject Category
Acoustics
Report/Patent Number
NF1676L-11519
Report Number: NF1676L-11519
Meeting Information
Meeting: NASA Acoustics Technical Working Group Meeting
Location: Hampton, VA
Country: US
Start Date: October 21, 2010
End Date: October 22, 2010
Sponsors: National Aeronautics and Space Administration
Funding Number(s)
WBS: 699959.02.10.07.06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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