A lamina is the basic building block of composite laminates. It can contain fibers of different materials and orientations. A laminate consists of multiple stacked laminae, each with potentially different thicknesses, fiber orientations, fiber materials, and matrix materials. Due to planes of material symmetry, laminae exhibit orthotropic behavior and have different material properties depending on the direction. Failure prediction for non-isotropic composite laminates, like unidirectional laminates, requires evaluating allowable stresses in the principal material directions rather than just maximum principal stresses due to varying material strengths by direction.
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Unidirectional fiber composite
1.
2. Unidirectional composite
• A lamina is the building block of modern
composite laminated structures.
• Each lamina may have in itself more than one
types of fibers. These fibers may be oriented
oriented in different different directions.
directions.
• A laminate has several layers, or laminae.
3. Each lamina may have a different:
– Thickness
– Fiber orientation angle
– Fiber material
– Matrix material
A lamina is also known as a ply, or a layer.
Each layer in a laminate has in general three planes of
material symmetry. Because Because of this, they exhibit
exhibit orthotropic orthotropic behavior behavior.
A lamina cut across these planes of symmetry will exhibit
same mechanical properties.
4.
5. • In isotropic materials, failure prediction requires
calculating principal stresses or Strain and
comparing them to allowable stress/strain limits
prescribed for the material.
• In non‐isotropic materials (e.g. transversely
isotropic materials), this approach does not work.
• The notion of Principal stress makes no sense for
these materials as material strength changes with
direction, and the direction of principal stress
may not in most of the cases coincide with
direction of maximum strength.
6. For unidirectional materials, we evaluate allowable
stress field in context of different strengths of
material in principal material directions. These
are:
– Longitudinal tensile strength
Lateral tensile strength
– Longitudinal compressive strength
Lateral compressive strength
– In‐plane shear strength