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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

  1. 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.
  2. 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.
  3. 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.
  4. 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.

Doubtly AI · 25 Oct 2026 AI-verified · Oct 2026 Report
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