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Rotor Broadband Noise Prediction with Comparison to Model DataThis paper reports an analysis and prediction development of rotor broadband noise. The two primary components of this noise are Blade-Wake Interaction (BWI) noise, due to the blades' interaction with the turbulent wakes of the preceding blades, and "Self" noise, due to the development and shedding of turbulence within the blades' boundary layers. Emphasized in this report is the new code development for Self noise. The analysis and validation employs data from the HART program, a model BO-105 rotor wind tunnel test conducted in the German-Dutch Wind Tunnel (DNW). The BWI noise predictions are based on measured pressure response coherence functions using cross-spectral methods. The Self noise predictions are based on previously reported semiempirical modeling of Self noise obtained from isolated airfoil sections and the use of CAMRAD.Modl to define rotor performance and local blade segment flow conditions. Both BWI and Self noise from individual blade segments are Doppler shifted and summed at the observer positions. Prediction comparisons with measurements show good agreement for a range of rotor operating conditions from climb to steep descent. The broadband noise predictions, along with those of harmonic and impulsive Blade-Vortex Interaction (BVI) noise predictions, demonstrate a significant advance in predictive capability for main rotor noise.
Document ID
20010050555
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Brooks, Thomas F.
(NASA Langley Research Center Hampton, VA United States)
Burley, Casey L.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Acoustics
Report/Patent Number
AIAA Paper 2001-2210
Report Number: AIAA Paper 2001-2210
Meeting Information
Meeting: 7th AIAA/CEAS Aeroacoustics Conference
Location: Maastricht
Country: Netherlands
Start Date: May 28, 2001
End Date: May 30, 2001
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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