From the mechanical properties of the composite listed in table 16 2 and the shear lag model the axial modulus of as4 3501 6 carbon epoxy cross ply laminate 0 90 2 s was calculated as a function of matrix crack density from equation 16 24 and compared with the experimental data as well as the results without the effects of residual thermal.
Carbon epoxy laminate density.
Volume fraction of fibres 55 60.
Composites density measurement void measurement carbon epoxy image analysis astm d792 voids porosity astm d1505 20.
Also excellent interlaminar and in plane shear strengths.
Thermal expansion coefficient longitudinal.
Properties carbon epoxy composite rod.
Young s modulus longitudinal.
Best tensile strength flexural modulus heat distortion temperature and linear expansion compared with other epoxy laminates.
The angle changes of the manufactured specimens were measured at room temperature 25oc by stamping the l section on a reference paper of right angle.
Properties carbon epoxy composite tube.
Compressive strength longitudinal.
Investigate the spring forward behavior of carbon epoxy composite laminate structures.
Carbon epoxy laminates of l section were manufactured by using an autoclave manufacturing process fig.