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TPSAS-NF1676L-36114-DNDA series of experiments were conducted in an anechoic hover chamber to investigate the noise and performance of an ideally twisted rotor design. The results of this test were compared with those of noise prediction tools.
Document ID
20200003243
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Nicole A Pettingill (Langley Research Center Hampton, Virginia, United States)
Nikolas S Zawodny (Langley Research Center Hampton, Virginia, United States)
Date Acquired
May 7, 2020
Publication Date
April 8, 2020
Subject Category
Acoustics
Report/Patent Number
NF1676L-36114
Report Number: NF1676L-36114
Meeting Information
Meeting: NASA Acoustics Technical Working Group
Location: Hampton, VA
Country: US
Start Date: April 12, 2018
Sponsors: National Aeronautics and Space Administration
Funding Number(s)
WBS: 664817.02.07.03.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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