EXPERIMENTAL CHARACTERIZATION OF FIVE PLIES HELIOPOL/STRATIMAT 300 COMPOSITE LAMINATE

Five plies of Heliopol 9431ATYX_LSE/Stratimat300 glass fabric (300 g/m^sup 2^ specific weight), 6 mm thick laminate has been considered for experimental characterization using the three-point bend tests. Following distributions have been experimentally determined on five layers of Heliopol 9431ATYX_LSE/Stratimat300 glass fabric specimens using data recorded by the materials testing machine: Load (N)-deflection (mm), Stiffness (N/m) of each specimen, Young's Modulus of Bending (MPa) of each specimen, Flexural Rigidity (Nm^sup 2^) according to each specimen, Maximum Bending Stress at Maximum Load (MPa)-Maximum Bending Strain at Maximum Load, Work to Maximum Load (Nmm) of each specimen, Load at Break (kN)-Deflection at Break (mm), Maximum Bending Stress at Break (MPa)- Maximum Bending Strain at Break and Work to Break (Nmm) of each specimen.