In this study, response of a flight vehicle component to rocket noise is considered. Tuned mass dampers, hitherto used in low frequency excitation, have been utilized to attenuate high frequency, broad band excitations. Modally tuned dampers have been investigated for a variety of input excitations. Modal dampers exhibit significant attenuation of all input signals. © 2010 Elsevier Masson SAS
This work explores the feasibility of using proof-mass actuators to actively control noise transmiss...
This paper presents a method to apply robust mass dampers on an industrial high-precision motion sta...
Effectiveness of multiple tuned mass dampers (MTMD) in suppressing the dynamic response of base exci...
AbstractRockets are subjected to vibrations in various operational phases. Source of vibration may b...
Vibration is a major problem in space launch vehicles during burning sequences. These vehicles are v...
Particle dampers provide a mechanism for diverting energy away from resonant structural vibrations. ...
Rocket motor generates vibrations acting on whole rocket body including its contents. Part of the bo...
In space launch vehicles, external excitation of the vehicle fairing by acoustic or structural loads...
Numerical optimisations were conducted to reduce the noise levels inside the payload bay of a rocket...
Particle dampers provide a mechanism for diverting energy away from resonant structural vibrations. ...
When equipment designs must perform in a broad band vibration environment it can be difficult to avo...
The analytical framework of a semi active tuned mass damper (SATMD) is developed for the reduction o...
Numerical optimisations were conducted to reduce the noise levels inside the payload bay of a rocket...
This paper presents the initial results of a simulation study on the flexural vibration and interior...
The optimum parameters of multiple tuned mass dampers (MTMD) for suppressing the dynamic response of...
This work explores the feasibility of using proof-mass actuators to actively control noise transmiss...
This paper presents a method to apply robust mass dampers on an industrial high-precision motion sta...
Effectiveness of multiple tuned mass dampers (MTMD) in suppressing the dynamic response of base exci...
AbstractRockets are subjected to vibrations in various operational phases. Source of vibration may b...
Vibration is a major problem in space launch vehicles during burning sequences. These vehicles are v...
Particle dampers provide a mechanism for diverting energy away from resonant structural vibrations. ...
Rocket motor generates vibrations acting on whole rocket body including its contents. Part of the bo...
In space launch vehicles, external excitation of the vehicle fairing by acoustic or structural loads...
Numerical optimisations were conducted to reduce the noise levels inside the payload bay of a rocket...
Particle dampers provide a mechanism for diverting energy away from resonant structural vibrations. ...
When equipment designs must perform in a broad band vibration environment it can be difficult to avo...
The analytical framework of a semi active tuned mass damper (SATMD) is developed for the reduction o...
Numerical optimisations were conducted to reduce the noise levels inside the payload bay of a rocket...
This paper presents the initial results of a simulation study on the flexural vibration and interior...
The optimum parameters of multiple tuned mass dampers (MTMD) for suppressing the dynamic response of...
This work explores the feasibility of using proof-mass actuators to actively control noise transmiss...
This paper presents a method to apply robust mass dampers on an industrial high-precision motion sta...
Effectiveness of multiple tuned mass dampers (MTMD) in suppressing the dynamic response of base exci...