Tone Noise Reduction of a Turbofan Engine by Additional Aerodynamical Blade Forces
Author:
Affiliation:
1. Technical University of Berlin
2. German Aerospace Center (DLR)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-3982
Reference22 articles.
1. H. H.;Groneweg J. F.,1991
2. Technology approach to aero engine noise reduction
3. Active control of the blade passage frequency noise level of an axial fan with aeroacoustic sound sources
4. Turbofan Tone Noise Reduction by Flow-Induced Unsteady Blade Forces
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2. Reduction of UHBR fan blade tones by flow induced secondary sound sources;22nd AIAA/CEAS Aeroacoustics Conference;2016-05-27
3. Sound emission of a turbine stage due to an azimuthally periodic mean temperature;International Journal of Aeroacoustics;2016-03
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