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Non-dimensional parameters which govern the maximum transverse displacement and first peak contact force in the laminated glass are proposed.
With increasing damping the peak of the maximum transverse displacement in the first unstable region decreases or even vanishes.
The postbuckling performance of composite laminated plates for a given compression loading is assessed by studying both the maximum transverse displacement and the end-shortening strain.
The validation was performed by comparing simulation results in term of the contact force, deformation shape, failure mode and the maximum transverse displacement with available published experimental test results by others.
The three point bending scheme is adopted for testing specimens, where an hydraulic actuator is used for the transmission of the transverse load at midspan under displacement control and an LVDT is used to measure the corresponding maximum transverse displacement.
The maximum transverse displacement of the vibrating screen is 0.13 mm, the maximum difference in vibration amplitude of corresponding points is 0.44mm and the maximum dynamic stress is 16.63MPa.
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Additionally, the pre-tension force results in decreasing of the maximum transverse displacements.
However, for exciting frequencies greater than that of the nanowire, maximum transverse displacements would increase or decrease with the magnetic field strength or electric current.
The effects of the magnetic field, electric current, pre-tension force, frequency of the applied load, surface and size effects on the maximum transverse displacements are discussed.
The obtained results display that for the frequency of the applied load lower than the nanowire׳s fundamental frequency, by increasing the magnetic field or electric current, the maximum transverse displacements would increase.
The objective of the present work is to predict the first-ply failure load, the ultimate failure load, the buckling load, the associated maximum transverse displacements, and locations and modes of failure of tapered laminated plates under the action of uni-axial compression.
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