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The flexibility and damage failure modes in composite materials introduce additional complexity for predicting hydrodynamic loads when interactive with water.
There is a need to study the behavior of the composite rotor system under various key damage modes in composite materials for developing Structural Health Monitoring (SHM) system.
A higher order displacement based formulation has been developed to investigate the plane strain edge vibrations or end modes in composite laminated sandwich plates.
The predictions are compared with experimental data obtained in pin- and bolt-loaded joints, and the results indicate that the methodology proposed can accurately and effectively predict ultimate failure loads as well as failure modes in composite bolted joints.
The prediction methods based on the characteristic lengths are validated by the tests for composite joints with different parameters, and the results indicate that the methodology proposed in this paper can accurately and effectively predict failure loads as well as failure modes in composite pre-tightened tooth.
Effects of the key damage modes in composite materials such as matrix cracking, debonding/delamination and fiber breakage on various properties of the composite rotor blade such as stiffnesses, frequencies, deflection, root forces, root moments and strains in forward flight are studied using an aeroelastic analysis.
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Possible failure modes in composites may include matrix cracking, fiber breakage, kinking, fiber-matrix debonding or delamination between composite plies.
Experimental conditions that promote a greenstick fracture mode in composite pultruded rods have been considered.
Delamination is the most common failure mode in composite materials, since it will result in the reduction of stiffness and can grow throughout other layers.
Delamination between plies is the most common failure mode in composite laminates that can cause fiber breakage and reduction in life of the composite.
The fatigue failure modes in SMA composite laminates were revealed.
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