NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Separation of Main and Tail Rotor Noise Sources from Ground-Based Acoustic Measurements Using Time-Domain De-DopplerizationA new method of separating the contributions of helicopter main and tail rotor noise sources is presented, making use of ground-based acoustic measurements. The method employs time-domain de-Dopplerization to transform the acoustic pressure time-history data collected from an array of ground-based microphones to the equivalent time-history signals observed by an array of virtual inflight microphones traveling with the helicopter. The now-stationary signals observed by the virtual microphones are then periodically averaged with the main and tail rotor once per revolution triggers. The averaging process suppresses noise which is not periodic with the respective rotor, allowing for the separation of main and tail rotor pressure time-histories. The averaged measurements are then interpolated across the range of directivity angles captured by the microphone array in order to generate separate acoustic hemispheres for the main and tail rotor noise sources. The new method is successfully applied to ground-based microphone measurements of a Bell 206B3 helicopter and demonstrates the strong directivity characteristics of harmonic noise radiation from both the main and tail rotors of that helicopter.
Document ID
20090035729
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Greenwood, Eric II
(NASA Langley Research Center Hampton, VA, United States)
Schmitz, Fredric H.
(Maryland Univ. College Park, MD, United States)
Date Acquired
August 24, 2013
Publication Date
September 22, 2009
Subject Category
Acoustics
Report/Patent Number
LF99-9186
Meeting Information
Meeting: 35th European Rotorcraft Forum 2009
Location: Hamburg
Country: Germany
Start Date: September 22, 2009
End Date: September 25, 2009
Funding Number(s)
WBS: WBS 877868.02.07.07.04.02
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available