Comparison of Predicted and Measured Attenuation of Turbine Noise from a Static Engine Test
Author:
Affiliation:
1. Goodrich Aerostructures Group
2. Pratt and Whitney
3. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-3533
Reference8 articles.
1. G.ZlavogandW.Eversman."SourceEffectsonRealizedAttenuationinLinedDucts",AIAAPaper2003-3247.
2. Nark, D. M., Farassat, F., Pope, D. S., and Vatsa, V."The Development of the Ducted Fan Noise Propagation and Radiation CodeCDUCT-LaRC", AIAA Paper 2003-1652.
3. E. W. Chien. "ATheoretical Study on AircraftEngine Acoustic Liner Optimization and Correlation with NASA Advanced Ducted Propulsor (ADP) Test",AIAA 2004 3032.
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. A Frequency Domain Model for Turbine Interaction Broadband Noise: Comparison with Measurements;2018 AIAA/CEAS Aeroacoustics Conference;2018-06-24
2. Aircraft noise prediction;Progress in Aerospace Sciences;2014-07
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