NASA NTRS · 19750026298
Analysis of twisting stiffness for a multifiber composite layer
Abstract
The twisting stiffness of a rectangular cross section consisting of a single row of solid circular cross-section fibers embedded in a matrix is analyzed. The problem is formulated as a Dirichlet torsion problem of a multielement region and solved by the boundary-point least-squares method. Numerical results for a single-fiber square cross section compare favorably with previous relaxation-method results. New numerical results for three and five-fiber composites suggest that the torsional rigidity of a multifiber composite can be approximated from the torsional rigidities of single and three-fiber models.
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Bert, C. W., Chang, S.. 1974-09-01. Analysis of twisting stiffness for a multifiber composite layer. https://ntrs.nasa.gov/citations/19750026298
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