Laminate elastic constants1 vf 56 8 58 2 tensile modulus el gpa 44 6 tensile modulus et gpa 17 0 tensile modulus ez gpa 16 7 compressive modulus el gpa 42 8 compressive modulus et gpa 16 0. Composite laminates may be regarded as a type of plate or thin shell structure and as such their stiffness properties may be found by integration of in plane stress in the direction normal to the laminates surface. The carbon fiber neat epoxy npef 170 composite laminate was also fabricated by the vartm technique as the control specimen.
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