Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1998.Includes bibliographical references (p. 165-170).The need for structural based acoustic control is evident in aircraft, aerospace, and naval systems. A promising approach utilizes active materials to intelligently control the dynamic response of light-weight, modally dense structures suppressing the radiated acoustic power. The basic representative structural element of a single panel offers an analytically tractable basis for examining various control methodologies for mitigating the acoustic response. An electro-mechanical Rayleigh-Ritz structural model is combined with an expression of the acoustic power radiated from a rectangular panel to yield ...
This paper investigates through numerical simulations the limits of performance for a class of feedf...
This paper presents a theoretical study comparing sound transmission through different kinds of smar...
The active ntroI of vibration using point tuators has received much attention especially for aircraf...
This work presents a comparison of three technologies for structural}acoustic control that, while pr...
An active structural acoustic control system for a composite fuselage type structure is developed in...
An active structural acoustic control system for a composite fuselage type structure is developed in...
This article is focused on the development and experimental realization of an active structural acou...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2002....
This paper compares the limitations of "optimal" feedforward and feedback strategies for active stru...
Composite materials are widely used in the aeronautic industry for their low mass/stiffness ratio. H...
Noise reduction in the transmission path of aircraft panels is a crucial step of enhanced designs f...
There has been considerable interest over the past several years in applying feedback control method...
Optimum placement of multiple traditional piezoceramic actuators is determined for active structural...
Optimum placement of multiple traditional piezoceramic actuators is determined for active structural...
Acoustic noise is an important problem in the modern society and provides much of the impetus for th...
This paper investigates through numerical simulations the limits of performance for a class of feedf...
This paper presents a theoretical study comparing sound transmission through different kinds of smar...
The active ntroI of vibration using point tuators has received much attention especially for aircraf...
This work presents a comparison of three technologies for structural}acoustic control that, while pr...
An active structural acoustic control system for a composite fuselage type structure is developed in...
An active structural acoustic control system for a composite fuselage type structure is developed in...
This article is focused on the development and experimental realization of an active structural acou...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2002....
This paper compares the limitations of "optimal" feedforward and feedback strategies for active stru...
Composite materials are widely used in the aeronautic industry for their low mass/stiffness ratio. H...
Noise reduction in the transmission path of aircraft panels is a crucial step of enhanced designs f...
There has been considerable interest over the past several years in applying feedback control method...
Optimum placement of multiple traditional piezoceramic actuators is determined for active structural...
Optimum placement of multiple traditional piezoceramic actuators is determined for active structural...
Acoustic noise is an important problem in the modern society and provides much of the impetus for th...
This paper investigates through numerical simulations the limits of performance for a class of feedf...
This paper presents a theoretical study comparing sound transmission through different kinds of smar...
The active ntroI of vibration using point tuators has received much attention especially for aircraf...