Effects of Bifurcations on Aft-Fan Engine Nacelle Noise
Author:
Affiliation:
1. NASA Langley Research Center
2. Analytical Services & Materials
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2988
Reference4 articles.
1. 2Dougherty,R.P.“AParabolicApproximationforFlowEffectsonSoundPropagationinNonuniform,Softwall, Ducts,”AIAAPaper99-1822,1999.
2. 4Nark,D.M.,Farassat,F.,Pope,D.S.,andVatsa,V.“AModelforShearLayerEffectsonEngineNoiseRadiation,”AIAAPaper2004-2992,2004.
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1. Inlet and Aft Tonal Noise Predictions of a Full-Scale Turbofan Engine with Bifurcation and Inlet Distortion;23rd AIAA/CEAS Aeroacoustics Conference;2017-06-02
2. Tonal Noise Prediction of a Turbofan with Heterogeneous Stator and Bifurcations;AIAA Journal;2015-11
3. Computational Aeroacoustics of Aft Fan Noises Characterizing a Realistic Coaxial Engine;AIAA Journal;2012-05
4. Hybrid Wing Body Aircraft System Noise Assessment with Propulsion Airframe Aeroacoustic Experiment;16th AIAA/CEAS Aeroacoustics Conference;2010-06-07
5. Synergism of flow and noise control technologies;Progress in Aerospace Sciences;2005-07
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