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Acoustic performance of an advanced model turbofan in three aeroacoustic test facilities
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Acoustic performance of the GEAE UPS research fan in the NASA Glenn 9- by 15-foot low-speed wind tunnel
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Aircraft engine technology for green aviation to reduce fuel burn
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Effect of two advanced noise reduction technologies on the aerodynamic performance of an ultra high bypass ratio fan
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NASA collaborative research on the ultra high bypass engine cycle and potential benefits for noise, performance, and emissions
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The effect of bypass nozzle exit area on fan aerodynamic performance and noise in a model turbofan simulator
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