On the application of a soft-vane cascade model in rotor-stator interaction noise prediction
Author:
Affiliation:
1. School of Energy and Power Engineering, Beihang University, China
2. Research Institute of Aero-Engine, Beihang University, China
Publisher
Gas Turbine Society of Japan
Link
https://www.jstage.jst.go.jp/article/jgpp/15/2/15_vol15no2tp04/_pdf
Reference13 articles.
1. Peake, N., and Parry, A. B., 2018, “Modern Challenges Facing Turbomachinery Aeroacoustics”, Annual Review of Fluid Mechanics, Vol. 44, pp. 227-248.
2. Hughes, C, E., and Gazzaniga, L., 2009, “Effect of Two Advanced Noise Reduction Technologies on the Aerodynamic Performance of an Ultra High Bypass Ratio Fan”, Proceedings, 15th AIAA/CEAS Aeroacoustics Conference, Miami, Florida, AIAA 2009-3139.
3. Elliott, D. M., Woodward, R, P., and Podboy G. G., 2009, “Acoustic Performance of Novel Fan Noise Reduction Technologies for a High Bypass Model Turbofan at Simulated Flights Conditions”, Proceedings, 15th AIAA/CEAS Aeroacoustics Conference, Miami, Florida, AIAA 2009-3140.
4. Jones, M. G., Parrott, T. L., Suliff, D. L., and Hughes, C, E., 2009, “Assessment of Soft Vane and Metal Foam Engine Noise Reduction Concepts”, Proceedings, 15th AIAA/CEAS Aeroacoustics Conference, Miami, Florida, AIAA 2009-3142.
5. Jones, M. G., and Howerton, B. M., 2016, “Evaluation of Novel Liner Concepts for Fan and Airframe Noise Reduction”, Proceedings, 22nd AIAA/CEAS Aeroacoustics Conference, Lyon, AIAA 2016-3787.
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