NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
A numerical study of active structural acoustic control in a stiffened, double wall cylinderIt is demonstrated that active structural acoustic control of complex structural/acoustic coupling can be numerically modeled using finite element and boundary element techniques in conjunction with an optimization procedure to calculate control force amplitudes. Appreciable noise reduction is obtained when the structure is excited at a structural resonance of the outer shell or an acoustic resonance of the inner cavity. Adding ring stiffeners as a connection between the inner and outer shells provides an additional structural transmission path to the interior cavity and coupled the modal behavior of the inner and outer shells. For the case of excitation at the structural resonance of the unstiffened outer shell, adding the stiffeners raises the structural resonance frequencies. The effectiveness of the control forces is reduced due to the off resonance structural response. For excitation at an acoustic cavity resonance, the controller effectiveness is enhanced.
Document ID
19950004865
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Grosveld, Ferdinand W.
(Lockheed Engineering and Sciences Co. Hampton, VA., United States)
Coats, T. J.
(Washington State Dept. of Transportation Olympia, WA., United States)
Lester, H. C.
(NASA Langley Research Center Hampton, VA, United States)
Silcox, R. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 17, 2013
Publication Date
January 1, 1994
Publication Information
Publication: Inst. of Noise Control Engineering, Noise Con 1994: Proceedings of the 1994 National Conference on Noise Control Engineering. Progress in Noise Control for Industry
Subject Category
Acoustics
Accession Number
95N11278
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.
No Preview Available