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Development of a Field-Deployable Microphone Phased Array for Airframe Noise Flyover MeasurementsThis technical memorandum describes in detail the construction and use of a large channel-count, field-deployable microphone phased array designed for airframe noise flyover measurements for a range of aircraft types and scales. The array incorporated 185 hardened, weather-resistant sensors suitable for outdoor use. A custom 4-mA current loop receiver circuit with temperature compensation was developed to power the sensors over extended cable lengths with minimal loss of signal-to-noise. Extensive calibrations and performance testing of the sensors were conducted to verify the design specifications. A compact data system combining sensor power, signal conditioning, and digitization was assembled for use with the array. Complementing the data system was a robust analysis system capable of near real-time presentation of beamformed and deconvolved contour plots and integrated spectra obtained from data acquired during flyover passes of the array. Additional instrumentation systems needed to process the array data were also developed, including a commercial 10-meter weather station comprised of a sonic anemometer, aspirated temperature/humidity probe and pressure sensor. Unique methods for assessing the health of the array in-situ were developed and demonstrated. A detailed mock-up of the instrumentation suite (phased array, weather station, and data processor) was performed in the NASA Langley Acoustic Development Laboratory in 2014 to vet the system performance. Issues with the sensors and electronics were identified during the mock-up and subsequently corrected. The array was then deployed for preliminary field testing at Fort A.P. Hill in Virginia in 2015 followed by the array being utilized in three separate full-scale airframe noise test campaigns at Edwards Air Force Base in California from 2016 to 2018 where the system was used to characterize the noise generated by both baseline and treated flaps and main landing gear on a commercial transport-sized vehicle.
Document ID
20230010620
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
William M Humphreys, Jr.
(Langley Research Center Hampton, Virginia, United States)
David P Lockard
(Langley Research Center Hampton, Virginia, United States)
Mehdi R Khorrami
(Langley Research Center Hampton, Virginia, United States)
William G Culliton
(Langley Research Center Hampton, Virginia, United States)
Robert G McSwain
(Langley Research Center Hampton, Virginia, United States)
Chester V Dolph
(Langley Research Center Hampton, Virginia, United States)
Patricio A Ravetta
(AVEC, Inc.)
Date Acquired
July 20, 2023
Publication Date
August 1, 2023
Subject Category
Acoustics
Report/Patent Number
NASA/TM-20230010620
Funding Number(s)
WBS: 981698.01.01.23.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Phased Array
Airframe Noise
Flyover Testing
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