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Beampattern control of a microphone array to minimize secondary source contamination
Peter Jordan1, John A Fitzpatrick, Craig Meskell
1Department of Mechanical Engineering, Trinity College, Dublin 2, Ireland.
The Journal of the Acoustical Society of America
|November 1, 2003
Summary
This study adapts null-steering to measure propeller noise on a model aircraft. The technique effectively isolated noise from one propeller, quantifying acoustic energy from the other.
Area of Science:
- Acoustics
- Aerodynamics
- Signal Processing
Background:
- Aeroacoustics is crucial for aircraft noise reduction.
- Measuring noise from individual components like propellers is challenging.
- Traditional beamforming methods may not isolate specific noise sources effectively.
Purpose of the Study:
- To adapt a null-steering technique for precise measurement of individual propeller noise.
- To quantify the acoustic energy generated by a single propeller on a twin-propeller aircraft model.
- To validate the effectiveness of the adapted null-steering method in aeroacoustic measurements.
Main Methods:
- Applied a null-steering technique to a linear delay-and-sum beamformer.
- Utilized array shading with weights derived from polynomial roots for null placement.
- Conditioned the cross-spectral matrix to mitigate directional aeroacoustic system effects.
- Employed a plane-wave formulation based on microwave antenna theory.
Main Results:
- Successfully steered nulls onto the second propeller, effectively isolating its acoustic contribution.
- Observed a 6 dB difference in measurements before and after null steering.
- Demonstrated the technique's efficacy in eliminating noise from one propeller.
- Provided a quantitative measure of acoustic energy from the remaining propeller.
Conclusions:
- The adapted null-steering technique is effective for isolating and measuring noise from individual propellers.
- Pre-conditioning the cross-spectral matrix is essential for accurate results with real-world aeroacoustic data.
- This method offers a valuable tool for detailed aeroacoustic analysis and noise source identification.