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Airframe Noise Results from the QTD II Flight Test ProgramWith continued growth in air travel, sensitivity to community noise intensifies and materializes in the form of increased monitoring, regulations, and restrictions. Accordingly, realization of quieter aircraft is imperative, albeit only achievable with reduction of both engine and airframe components of total aircraft noise. Model-scale airframe noise testing has aided in this pursuit; however, the results are somewhat limited due to lack of fidelity of model hardware, particularly in simulating full-scale landing gear. Moreover, simulation of true in-flight conditions is non-trivial if not infeasible. This paper reports on an investigation of full-scale landing gear noise measured as part of the 2005 Quiet Technology Demonstrator 2 (QTD2) flight test program. Conventional Boeing 777-300ER main landing gear were tested, along with two noise reduction concepts, namely a toboggan fairing and gear alignment with the local flow, both of which were down-selected from various other noise reduction devices evaluated in model-scale testing at Virginia Tech. The full-scale toboggan fairings were designed by Goodrich Aerostructures as add-on devices allowing for complete retraction of the main gear. The baseline-conventional gear, faired gear, and aligned gear were all evaluated with the high-lift system in the retracted position and deployed at various flap settings, all at engine idle power setting. Measurements were taken with flyover community noise microphones and a large aperture acoustic phased array, yielding far-field spectra, and localized sources (beamform maps). The results were utilized to evaluate qualitatively and quantitatively the merit of each noise reduction concept. Complete similarity between model-scale and full-scale noise reduction levels was not found and requires further investigation. Far-field spectra exhibited no noise reduction for both concepts across all angles and frequencies. Phased array beamform maps show inconclusive evidence of noise reduction at selective frequencies (1500 to 3000 Hz) but are otherwise in general agreement with the far-field spectra results (within measurement uncertainty).
Document ID
20070021691
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Elkoby, Ronen
(Boeing Co. Seattle, WA, United States)
Brusniak, Leon
(Boeing Co. Seattle, WA, United States)
Stoker, Robert W.
(Boeing Co. Seattle, WA, United States)
Khorrami, Mehdi R.
(NASA Langley Research Center Hampton, VA, United States)
Abeysinghe, Amal
(Goodrich Corp. Chula Vista, CA, United States)
Moe, Jefferey W.
(Goodrich Corp. Chula Vista, CA, United States)
Date Acquired
August 23, 2013
Publication Date
May 21, 2007
Subject Category
Acoustics
Report/Patent Number
AIAA 2007-3457
Report Number: AIAA 2007-3457
Meeting Information
Meeting: 13th AIAA/CEAS Aeroacoustics Conference
Location: Rome
Country: Italy
Start Date: May 21, 2007
End Date: May 23, 2007
Sponsors: National Oceanic and Atmospheric Administration, American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 561581.02.08
Distribution Limits
Public
Copyright
Public Use Permitted.
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