Accession Number : ADA305580

Title :   10 Degree Off-Axis Tensile Test for Intralaminar Shear Characterization of Fiber Composites.

Descriptive Note : Technical note,

Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION CLEVELAND OH LEWIS RESEARCH CEN TER

Personal Author(s) : Chamis, Christos C. ; Sinclair, John H.

PDF Url : ADA305580

Report Date : APR 1976

Pagination or Media Count : 33

Abstract : A combined theoretical and experimental investigation was conducted to assess the suitability of the 10 deg off-axis tensile test specimen for the intralaminar shear characterization of uni- directional composites. Composite mechanics, a combined-stress failure criterion, and a finite element analysis were used to determine theoretically the stress-strain variation across the specimen width and the relative stress and strain magnitudes at the 10 deg plane. Strain gages were used to measure the strain variation across the specimen width at specimen midlength and near the end tabs. Specimens from Mod-I/epoxy, T-300/epoxy, and S-glass/ epoxy were used in the experimental program. It was found that the 10 deg off-axis tensile test specimen is suitable for intralaminar shear characterization and it is recommended that it should be considered as a possible standard test specimen for such a characterization. (MM)

Descriptors :   *STRESS ANALYSIS, *LAMINATES, *FIBER REINFORCED COMPOSITES, *TENSILE TESTERS, STRESS STRAIN RELATIONS, COMPOSITE MATERIALS, FINITE ELEMENT ANALYSIS, ORIENTATION(DIRECTION), FABRICATION, FRACTURE(MECHANICS), SHEAR STRESSES, STRAIN GAGES, EPOXY COMPOSITES, FAILURE(MECHANICS), AXIAL LOADS, DIRECTIONAL.

Subject Categories : Plastics
      Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE