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Advanced noise control fan aerodynamic performance
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Aeroacoustic experiments with twin jets
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Inlet acoustic data from a high bypass ratio turbofan rotor in an internal flow component test facility
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Orifice mass flow calculation in NASA's W-8 single stage axial compressor facility
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The aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor
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The impact of subsonic twin jets on airport noise
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