Composite reliability enhancement via preloading.
Jones, Mark Christopher
Wu, Edward M.
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Composite strength is an inverse function of the size of the composite. As the use of composites expands into larger applications, such as airplane wings, missile components, and ship superstructures, the ability to accurately predict composite performance for large applications has become more important. The composite failure process is sequential and initiates with early breaking of the weak fibers. Concentration of breakage sites accumulates and leads to ultimately catastrophic failure. Prestressing fibers prior to solidification of the matrix has been demonstrated to increase the reliability of the composite by minimizing the spatial concentration of the breakage sights. This study concentrates on quantifying the level of preload and gauge length to optimize the prestress effect. Computer simulations of graphite bundle tests were used to validate the data analysis methodologies applied to actual AS-4 graphite bundle tests. The actual experimental results are consistent with computer-simulated behaviors.
RightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.
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