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タイトルScreening of Potential Landing Gear Noise Control Devices at Virginia Tech For QTD II Flight Test
本文(外部サイト)http://hdl.handle.net/2060/20070023559
著者(英)Khorrami, Mehdi R.; Stoker, Robert W.; Ravetta, Patricio A.; Burdisso, Ricardo A.; Ng, Wing F.
著者所属(英)Virginia Polytechnic Inst. and State Univ.; NASA Langley Research Center
発行日2007-05-21
言語eng
内容記述In support of the QTD II (Quiet Technology Demonstrator) program, aeroacoustic measurements of a 26%-scale, Boeing 777 main landing gear model were conducted in the Virginia Tech Stability Tunnel. The objective of these measurements was to perform risk mitigation studies on noise control devices for a flight test performed at Glasgow, Montana in 2005. The noise control devices were designed to target the primary main gear noise sources as observed in several previous tests. To accomplish this task, devices to reduce noise were built using stereo lithography for landing gear components such as the brakes, the forward cable harness, the shock strut, the door/strut gap and the lower truck. The most promising device was down selected from test results. In subsequent stages, the initial design of the selected lower truck fairing was improved to account for all the implementation constraints encountered in the full-scale airplane. The redesigned truck fairing was then retested to assess the impact of the modifications on the noise reduction potential. From extensive acoustic measurements obtained using a 63-element microphone phased array, acoustic source maps and integrated spectra were generated in order to estimate the noise reduction achievable with each device.
NASA分類Aircraft Design, Testing and Performance
レポートNOAIAA Paper No. 2007-3455
権利Copyright, Distribution as joint owner in the copyright


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