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The mechanisms of airspace injury that mediate adverse patterns of mechanical ventilation include stretching of open lung units, amplified tangential (shearing) forces at the interface between open and closed lung units, and the recurring small airway trauma of tidal breathing.
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Polymer melts are fluids, which means they flow under the application of a tangential (shear stress).
Navier [6] in 1827 first proposed a partial slip condition for rough surfaces, relating the tangential velocity to the local tangential shear stress.
The matrix equivalent stresses, however, are not significantly affected by tangential shear sliding until normal interface separation occurs.
During transverse loading of fiber-matrix composites, the interface is subjected to both tangential shear stresses and radial stresses.
During transverse loading of continuous fibre-reinforced composites, large tangential shear stresses develop at the interface at about 45° to the loading axis.
Results indicate that stress redistribution due to tangential shear sliding may significantly modify both interface radial stress distribution and matrix hoop stress.
A methodology and pertinent plots are provided for determining the stress concentration factor and the normal bond strength of an interface where tangential shear sliding is known to occur.
Comparison of these results with experimental observations and finite element analysis of transverse tension tests indicates that failure in SCS-6/Ti-6Al-4V and Acomposites4V composises initiatedted by tangential shear failure of the interface.
In the present study, an attempt has been made to measure the tangential shear strength of the interface for single fibre SiC/Ti-6Al-4V composites with varying interfaces using torsion testing and finite element stress analysis.
The present results have been validated through numerical tests which confirm zero tangential shear at the free-surface and comparisons with experimental observations of cavity and vortex ring formation underneath the impact location.
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