FJ44 Turbofan Engine Test at NASA Glenn Research Center's Aero-Acoustic Propulsion Laboratory
Author:
Affiliation:
1. Sierra Lobo, Inc
2. NASA Glenn Research Center
3. Williams International
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-620
Reference5 articles.
1. A Large Hemi-anechoic Enclosure for Community-Compatible Aeroacoustic Testing of Aircraft Propulsion Systems
2. Buckley,J.L."ContainmentShieldDesignforWilliamsInternationalFJ44-3EngineinAero-Acoustic Propulsion Laboratory at NASA Glenn",ASRC Task #NNC08E271T
3. Sutliff,D.L."RotatingRakeModeMeasurementSystem",NASATM-2005-213828.
Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. High-Speed Turbofan Noise Reduction Using Foam-Metal Liner Over-the-Rotor;Journal of Aircraft;2013-09
2. Phased Array Noise Source Localization Measurements Made on a Williams International FJ44 Engine;15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference);2009-05-11
3. Attenuation of FJ44 Turbofan Engine Noise with a Foam-Metal Liner Installed Over-the-Rotor;15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference);2009-05-11
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