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Contra-Rotating Open Rotor Tone Noise PredictionReliable prediction of contra-rotating open rotor (CROR) noise is an essential element of any strategy for the development of low-noise open rotor propulsion systems that can meet both the community noise regulations and cabin noise limits. Since CROR noise spectra exhibit a preponderance of tones, significant efforts have been directed towards predicting their tone content. To that end, there has been an ongoing effort at NASA to assess various in-house open rotor tone noise prediction tools using a benchmark CROR blade set for which significant aerodynamic and acoustic data have been acquired in wind tunnel tests. In the work presented here, the focus is on the nearfield noise of the benchmark open rotor blade set at the cruise condition. Using an analytical CROR tone noise model with input from high-fidelity aerodynamic simulations, tone noise spectra have been predicted and compared with the experimental data. Comparisons indicate that the theoretical predictions are in good agreement with the data, especially for the dominant tones and for the overall sound pressure level of tones. The results also indicate that, whereas the individual rotor tones are well predicted by the combination of the thickness and loading sources, for the interaction tones it is essential that the quadrupole source is also included in the analysis.
Document ID
20150002338
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Envia, Edmane
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
March 3, 2015
Publication Date
June 16, 2014
Subject Category
Acoustics
Aircraft Design, Testing And Performance
Aerodynamics
Report/Patent Number
GRC-E-DAA-TN15044
Report Number: GRC-E-DAA-TN15044
Meeting Information
Meeting: AIAA/CEAS Aeroacoustics Conference
Location: Atlanta, GA
Country: United States
Start Date: June 16, 2014
End Date: June 20, 2014
Sponsors: American Inst. of Aeronautics and Astronautics, Council of European Aerospace Societies
Funding Number(s)
WBS: WBS 473452.02.03.07.06.01.08
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Propeller Noise
Noise Prediction
Aerodynamic Noise
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