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- W619626918 abstract "In order to use filamentary composites as a replacement for steel in automotive structures, an analytical study was undertaken to determine a transition geometry between a graphite/epoxy laminate cylinder and E-glass/epoxy cylindrical tabs which would minimize stress concentrations in the transition area. Axisymmetric anisotropic finite element analyses were performed to determine stress concentrations during in-plane loading, single and combined, of a series of end tab materials, end tab designs, and configurations for the steel grips at each end of the tubular structure. It was found that extreme stress concentrations can occur in the areas of load transfer for tubular composites. Geometric discontinuities causing abrupt changes in the circumferential stiffness can cause axial bending stresses to reach a critical level while circumferential stresses are still low. Pressure compensation on the tubular ends can help reduce these stress concentrations. This is best performed by increasing the circumferential stiffness from the tubular specimen to the end tabs and from end tabs to grips as gradually as possbile, using a combination of intermediate softer materials and geometries free from sharp discontinuities." @default.
- W619626918 created "2016-06-24" @default.
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- W619626918 date "1980-01-01" @default.
- W619626918 modified "2023-09-24" @default.
- W619626918 title "LOAD INTRODUCTION PROBLEMS WITH TUBULAR COMPOSITE STRUCTURAL MEMBERS" @default.
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