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Acoustic Testing of the Tiltrotor Test Rig in the National Full-Scale Aerodynamics Complex 40- by 80-Foot Wind TunnelThe Tiltrotor Test Rig (TTR) was tested in the National Full-Scale Aerodynamics Complex (NFAC) 40- by 80-Foot Wind Tunnel from 2017 to 2018. The rotor system can be configured in airplane mode, with the rotor plane perpendicular to the wind flow, and in helicopter mode, with the rotor plane parallel to the wind flow. Four microphones were placed around the TTR: two on the wind tunnel floor and two on struts. The primary goal of the test was to understand the operational capabilities of the TTR, while also acquiring research data as available. Limited measurements of the blade vortex interaction (BVI) noise of the TTR rotor were taken to not only understand the acoustic testing capabilities of the TTR in the NFAC 40- by 80-Foot Wind Tunnel, but to also compare to previous tests and to be used for future validation studies. In particular, data will be compared to measurements of an XV-15 rotor previously acquired in the NFAC 80- by 120-Foot Wind Tunnel.
Document ID
20190025111
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Schatzman, Natasha L.
(NASA Ames Research Center Moffett Field, CA, United States)
Malpica, Carlos
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
May 15, 2019
Publication Date
May 13, 2019
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
ARC-E-DAA-TN62155
Meeting Information
Meeting: Vertical Flight Society''s Annual Forum and Technology Display
Location: Philadelphia, PA
Country: United States
Start Date: May 13, 2019
End Date: May 16, 2019
Sponsors: Vertical Flight Society
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Tiltrotor Test Rig
40- by 80-Foot Wind Tunnel
Acoustics Testing
National Full-Scale Aerodynamics Complex
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