In the design of lightweight structures, the construction of damping still is an unused design freedom. While material inherent damping of aluminum or composite materials is generally low, the internal damping of elastomers is significant. The basic concept of including local elastomer dampers into aluminum or composite components of aeronautic structures is addressed with the objective to increase the damping of specific vibration modes. The modelling from 1D rheological models of visco-elastic material up to 2D and 3D modelling using finite elements is addressed. Using the finite element method, a global damping matrix can be generated which enables forecasts of modal damping levels. A parameter study on a simple dynamic oscillator has be...
The employment of viscoelastic materials for the passive control of noise and vibration transmitted ...
Composite materials have been used in the design of the aircrafts structures because their low weigh...
The goal of this ongoing initial study is to model the critical behaviors of rotorcraft elastomeric ...
Due to their low mass and stiffening components like frames, stringers and panels, aircraft fuselage...
Structural vibrations often cause problems in high precision instruments, which may be solved by int...
Structural vibrations often cause problems in high precision instruments, which may be solved by int...
The effect of the damping addition due to viscoelastic (VE) material on the dynamic behavior of alum...
This paper deals with an evaluation of intrinsic vibration damping properties of structural material...
Abstract. In the present paper, the damping study of composites is approached from the viewpoint of ...
As lightweight and stiffened structures, aircraft are prone to vibration. Constrained Layer Damping ...
Many new viscoelastic materials have been developed recently to help improve noise and vibration lev...
This project work expresses the difference between the structures with and without damping material....
SIGLECopy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ - Fachinformationszzentrum Kar...
To add damping to the system, viscoelastic materials (VEM) are added to structures, in order to enha...
Engineering preliminary design methods for approximating and predicting the effects of viscous or eq...
The employment of viscoelastic materials for the passive control of noise and vibration transmitted ...
Composite materials have been used in the design of the aircrafts structures because their low weigh...
The goal of this ongoing initial study is to model the critical behaviors of rotorcraft elastomeric ...
Due to their low mass and stiffening components like frames, stringers and panels, aircraft fuselage...
Structural vibrations often cause problems in high precision instruments, which may be solved by int...
Structural vibrations often cause problems in high precision instruments, which may be solved by int...
The effect of the damping addition due to viscoelastic (VE) material on the dynamic behavior of alum...
This paper deals with an evaluation of intrinsic vibration damping properties of structural material...
Abstract. In the present paper, the damping study of composites is approached from the viewpoint of ...
As lightweight and stiffened structures, aircraft are prone to vibration. Constrained Layer Damping ...
Many new viscoelastic materials have been developed recently to help improve noise and vibration lev...
This project work expresses the difference between the structures with and without damping material....
SIGLECopy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ - Fachinformationszzentrum Kar...
To add damping to the system, viscoelastic materials (VEM) are added to structures, in order to enha...
Engineering preliminary design methods for approximating and predicting the effects of viscous or eq...
The employment of viscoelastic materials for the passive control of noise and vibration transmitted ...
Composite materials have been used in the design of the aircrafts structures because their low weigh...
The goal of this ongoing initial study is to model the critical behaviors of rotorcraft elastomeric ...