In one line
Fibre-reinforced composites contain strong, stiff fibres embedded in a matrix; their strength depends heavily on fibre length, orientation, volume fraction and the fibre–matrix bond.
Explained simply
A rope of many threads is strong when you pull it along its length, but you can easily separate the threads sideways. Fibre composites behave the same way: very strong along the fibres, weaker across them. And just as a short bit of tape doesn't stick well, very short fibres cannot pick up the full load from the matrix.
How it works
- Load applied to the composite is transferred by shear from the matrix to the fibre along its length. The fibre end portions carry less load.
- There is a critical fibre length lc. If fibre length ≫ lc (roughly more than 15 lc), the fibre behaves as continuous and is fully effective. Shorter fibres give less reinforcement.
- Orientation:
- Continuous aligned: maximum strength and stiffness along fibres (anisotropic).
- Discontinuous aligned: good strength along one direction, easier processing.
- Discontinuous random: nearly isotropic in the plane, lower strength.
- Laminates with layers at 0°/90°/±45° give balanced properties in many directions.
- Common fibres: glass (cheap, good strength, most widely used), carbon (very high stiffness and strength, light, costly), aramid/Kevlar (very tough, high impact and cut resistance), natural fibres (jute, coir, sisal; cheap and renewable).
Key formula
\( l_c = \dfrac{\sigma_f\, d}{2\,\tau_c} \)
- \( l_c \) = critical fibre length
- \( \sigma_f \) = tensile strength of the fibre (MPa)
- \( d \) = fibre diameter
- \( \tau_c \) = fibre–matrix bond strength or matrix shear yield strength (MPa)
Longitudinal modulus (continuous aligned): \( E_c = E_m V_m + E_f V_f \).
Quick example
Glass fibre with σf = 3000 MPa and d = 10 μm in a matrix with τc = 30 MPa: lc = 3000 × 10 / (2 × 30) = 500 μm (0.5 mm). Fibres much longer than 0.5 mm reinforce efficiently.
Applications: GFRP in water tanks, pipes, boat hulls and car body parts; CFRP in aircraft wings, racing cars, bicycle frames, prosthetics; Kevlar composites in body armour and helmets.
Common mistakes
- Assuming a fibre composite is equally strong in all directions.
- Thinking any fibre length gives full reinforcement; below lc the effect is small.
- Ignoring the interface; poor bonding lets fibres pull out.
How MU asks it
"Write a short note on fibre-reinforced composites" (3–5 marks) as part of classification questions. For full marks: definition, role of fibre length (critical length) and orientation (with a sketch of aligned vs random), names of common fibres with one property and one application each.