Click on images for details

 

Solid Finite Element Modeling of structural assemblies

Solid Finite Element modeling is employed to provide high-fidelity representation of the explored concepts and realistic prediction of structural behavior. A combined Matlab-Abaqus environment has been devised for this purpose, which generates 2D and 3D structural assemblies featuring arbitrarily complicated geometries in an automated and fully parametrized fashion. Geometry and material parameters are provided as inputs to a Matlab script, which produces an ASCII file in the Abaqus .jnl format. This file contains a description of operations required for Abaqus to generate the desired structure. The procedure is illustrated in Figure 1.

Figure 1: Combined Matlab-Abaqus environment for generation of solid FE models of relevant structural assemblies.

IAIR concept implementation

Practical realizations of IAIR and chiral cells for structural assemblies are being designed and analyzed with the implemented solid modeling environment. The concepts of vibration control through internal resonators and through viscoelastic damping are combined by employing viscoelastic materials in the realization of elementary cells. An IAIR-based design under investigation is shown in Figure 2(a). The assembly is composed by an aluminum box beam representing the backbone structure, filled with a lattice of IAIR-based unit cells. Ligaments of these cells are made of a rubber-like viscoelastic material, while steel cylinder inclusions are used as resonating masses.  The tip frequency response of the assembly in a clamped-free configuration is plotted in Figure 2(b). Simulations predict strong attenuation of the outer frame vibration around its first natural frequency when the resonating system is inserted.

Figure 2: (a) Structural assembly with box beam and visco-IAIR lattice inclusion. (b) Tip frequency response of the box beam before (blue) and after (red) insertion of the resonating system.

Chiral concept implementations

Using a similar approach to that described above, structural assemblies composed of a box beam and inclusions in the shapes of chiral lattices with different properties are currently under investigation. Figure 3 shows four different designs: (a) uniform-size chiral lattice, (b) lattice with graded masses, (c) anisotropic (stretched) lattice with lightweight annular masses, and (d) anisotropic lattice with graded masses. Cell ligaments in all lattices are made of a viscoelastic material. Corresponding frequency responses predicted by FEM simulations are reported in Figure 3(e). Wide bandgaps at moderately high frequency are produced by almost all configurations, while different degrees of vibration control at low frequencies are achieved, as can be seen from the zoomed view of Figure 3(f). For example, design (c) provides the flattest response in the [0, 20] Hz range, while design (d) allows for vibration damping over a very wide frequency range. So a class of different assemblies can be devised to meet a broad range of specifications.

Figure 3: (a)-(d) Visco-chiral assemblies. (e) Corresponding frequency responses compared to that of the box beam without inclusions (blue line). (f) Zoomed view of (e) in the [0, 50] Hz range.

Georgia Institute of Technology – School of Aerospace Engineering

 Atlanta, Georgia 30332-0150

Contact Us:

Massimo Ruzzane

Emanuele Baravelli

ruzzene@gatech.edu

ebaravelli@gatech.edu