Local feedback control of light honeycomb panels

Journal of the Acoustical Society of America

Volumn 121, Issue 1, 2007, Pages 222-233

  Hong, Chinsuk ^a   Elliott, Stephen J ^a  

^a UNIVERSITY OF SOUTHAMPTON   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC WAVE TRANSMISSION; ACTUATORS; HONEYCOMB STRUCTURES; STRUCTURAL DESIGN; STRUCTURAL PANELS;

HONEYCOMB PANELS; LOCALIZATION; MULTICHANNEL ACTIVE CONTROL; PIEZOCERAMIC ACTUATORS;

FEEDBACK CONTROL;

AIRCRAFT; ARTICLE; CERAMICS; EXPERIMENTAL MODEL; FEEDBACK SYSTEM; NOISE REDUCTION; PRIORITY JOURNAL; SENSOR; SOUND DETECTION; SOUND TRANSMISSION; THEORETICAL MODEL;

ACOUSTICS; AIRCRAFT; CERAMICS; HUMANS; MODELS, THEORETICAL; NOISE, TRANSPORTATION; VIBRATION;

EID: 33846206916     PISSN: 00014966     EISSN: None     Source Type: Journal    
DOI: 10.1121/1.2384843     Document Type: Article

References (26)

1. Barton, C. K., and Mixson, J. S. (1981). " Noise transmission and control for a light twin-engine aircraft., " J. Aircr. 18, 570-575.
2. Bhat, W. V. (1999). " Flight test measurement of exterior turbulent boundary layer pressure fluctuations on Boeing model 737 airplane., " J. Sound Vib. 14, 439-457.
3. Fahy, F., and Walker, J. (2004). Advanced Applications in Acoustics, Noise and Vibration (Spon, London).
4. Fuller, C. R., Elliott, S. J., and Nelson, P. A. (1996). Active Control of Vibration (Academic, London).
5. Gardonio, P. (2002). " Review of active technique for aerospace vibro-acoustic control., " J. Aircr. 39, 206-214.
6. Gardonio, P., and Elliott, S. J. (1999). " Active control of structure-borne and airborne sound transmission through double panel., " J. Aircr. 36, 1023-1032.
7. Hong, C. (2005). " Active control of resiliently mounted flexible structures., " Ph.D. thesis, Institute of Sound and Vibration, University of Southampton, UK.
8. Hong, C., and Elliott, S. J. (2005). " Active control of resiliently-mounted beams with a moment pair., " Smart Mater. Struct. 14, 727-738.
9. Leissa, A. W. (1969). Theory of Plates (NASA).
10. Malker, H. (1999). " Active damping of impacts in panels., " Master's thesis, Institute of Sound and Vibration, University of Southampton, UK.
11. Maury, C., Gardonio, P., and Elliott, S. J. (2002). " Model for active control of flow-induced noise transmitted through double partitions., " AIAA J. 40, 1113-1121.
12. Mixson, J. S., and Powell, C. A. (1984). " Review of recent research on interior noise of propeller aircraft., " AIAA/NASA 9th Aeroacoustics Conference, Williamsburg, VA.
13. Mixson, J. S., and Wilby, J. F. (1995). Interior Noise, Aeroacoustics of Flight Vehicles, Theory and Practice, edited by, H. H. Hubbard, (NASA Langley Research Center).
14. Mixson, J. S., Barton, C. K., and Vaicatis, R. (1978). " Investigation of interior noise in a twin-engine light aircraft., " J. Aircr. 15, 227-233.
15. Nelson, P. A., and Elliott, S. J. (1992). Active Control of Sound (Academic, New York).
16. Nilsson, E., and Nilsson, A. C. (2002). " Prediction and measurement of some dynamic properties of sandwich structures with honeycomb and foam cores., " J. Sound Vib. 251, 409-430.
17. Pope, L. D., Wilby, E. G., and Wilby, J. F. (1987a). " Propeller aircraft interior noise model. I. Theoretical model., " J. Sound Vib. 118, 449-467.
18. Pope, L. D., Willis, C. M., and Mayes, W. (1987b). " Propeller aircraft interior noise model. II. Scale-model and flight-test comparison., " J. Sound Vib. 118, 469-493.
19. Reddy, J. N. (1996). Mechanics of Laminated Composite Plates (CRC Press, Boca Raton, FL).
20. Saito, T., Parbery, R. D., Okuno, S., and Kawano, S. (1997). " Parameter identification for aluminum honeycomb sandwich panels based on orthotropic Timoshenko beam theory., " J. Sound Vib. 208 (2), 271-287.
21. Stothers, I. (2004). Personal communications.
22. Sulc, J., Hofr, J., and Benda, L. (1982). " Exterior noise on the fuselage of light propeller driven aircraft in flight., " J. Sound Vib. 84, 105-120.
23. Unruh, J. F. (1988). " Structure-borne noise control for propeller aircraft., " J. Aircr. 17, 752-757.
24. Unruh, J. F. (1989). " Installation effects on propeller wake/vortex-induced structure-borne noise transmissions., " J. Aircr. 27, 444-448.
25. Vaicatis, R. (1980). " Noise transmissions into a light aircraft., " J. Aircr. 17, 81-86.
26. Warburton, G. B. (1951). " The vibration of rectangular plates., " Proc. Inst. Mech. Eng. 168, 371-384.