Moreover, you have multiple options of different laminate finishes to upgrade the look of your hospital flooring.
The fatigue crack growth (FCG) behavior of five different laminate orientations ([0/90]2s, [90/0]2s, [±45]2s, [150/60]2s and [60/150]2s) of cross-ply Ti 6Al 4V/SCS-6 has been investigated at room temperature in air.
Drop-weight impact tests were conducted to induce cracking of the FMLs, and the crack initiation along with crack propagation behavior of the different laminate sequences ([0/0], [0/90], [0/90/0], [90/0/90] and [0/90/90/0]) were also studied.
The comparison between the results revealed markedly different behaviors among different laminates due to the bend twist coupling effects.
Therefore, we investigated the degradation behavior of laminates with different designs, including laminate types with an open, thus breathable, front-side and two standard designs with one or two layers of EVA in front of the cell, respectively.
This paper presents a detailed investigation about the geometric non-linear stiffness behavior of corrugated laminates in six different load cases.
For experimental investigation, the fracture behavior of interleaved laminates has been determined by Double Cantilever Beam (DCB) tests using two different thicknesses of membrane.
Previously, this test set-up was employed to determine interlaminar fracture behavior of composite laminates [27].
This paper presents a detailed investigation about the vibration behavior of corrugated laminates.
One cannot properly describe or model the behavior of composite laminates, therefore, without an understanding and representation of nonlinear behavior.
