Flight test of ASAC aircraft interior noise control system
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
2. NRC, Hampton, VA
3. U.S. Army, Research Lab., Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-1933
Reference19 articles.
1. Experiments on reduction of propeller induced interior noise by active control of cylinder vibration
2. Piezoelectric Actuator Models for Active Sound and Vibration Control of Cylinders
3. Mechanisms of active noise control by vibration sources
4. D. R. Thomas, P. A. Nelson, and S. J. Elliott. Active control of the transmission of sound through a thin cylindrical shell, part II: The minimization of acoustic potential energy. Journal of Sound and Vibration, 167(l): 113-128,1993.
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1. Active Wing Load Alleviation with an Adaptive Feed-forward Control Algorithm;AIAA Guidance, Navigation, and Control Conference and Exhibit;2006-06-15
2. Vibration Absorbers: A Review of Applications in Interior Noise Control of Propeller Aircraft;Journal of Vibration and Control;2004-08
3. Beech 1900D flight test to characterize propeller noise on the fuselage exterior;7th AIAA/CEAS Aeroacoustics Conference and Exhibit;2001-05-28
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