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Acoustic Testing of the Bell 699 Rotor on the Tiltrotor Test Rig (TTR) in the National Full-Scale Aerodynamics Complex 40- by 80- Foot Wind Tunnel in Conversion and Airplane ConfigurationThe Tiltrotor Test Rig (TTR) provides new proprotor testing capabilities to the National Aeronautics and Space Administration (NASA) and the Department of Defense (DoD). A checkout test for the TTR with the 699 proprotor was performed in the National Full-Scale Aerodynamics Complex (NFAC) 40- by 80 Foot Wind Tunnel from 2017 to 2018. Four microphones were placed around the rotor to capture acoustic data. Revolution based acoustic data processing techniques are evaluated for appropriateness in both helicopter and airplane configurations. This paper presents the acoustic data acquired for the rotor in conversion and airplane configuration.
Document ID
20200000541
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Shelts, Kelly
(Wichita State Univ. Wichita, KS, United States)
Schatzman, Natasha
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
January 27, 2020
Publication Date
January 21, 2020
Subject Category
Acoustics
Report/Patent Number
ARC-E-DAA-TN77280
Report Number: ARC-E-DAA-TN77280
Meeting Information
Meeting: Transformative Vertical Flight 2020
Location: San Jose, CA
Country: United States
Start Date: January 21, 2020
End Date: January 23, 2020
Sponsors: Vertical Flight Society
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
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