Definitions
Structure & Mechanics
Types of Composites
Applications
Limitations & Failure
100

A material made from two or more distinct materials that remain separate at a macroscopic level

Composite material

100

The force transfer mechanism from matrix to fibres in a fibre-reinforced composite

Shear forces at the matrix–fibre interface

100

Concrete is an example of this type of composite

Particle-reinforced composite

100

A reason composites are used in bicycle frames

Lightweight and strong

100

The type of failure where fibres pull out of the matrix

Fibre pull-out failure

200

The component in a composite that binds the structure together and transfers load

Matrix
200

The effect of aligning fibres parallel to the applied force

Maximum tensile strength and stiffness

200

Carbon fibre reinforced polymer belongs to this class of composites

Fibre-reinforced polymer (FRP)

200

An advantage of composites in aerospace engineering

High strength-to-weight ratio / fuel efficiency  

200

Why cracks in composites often stop rather than propagate easily

Crack energy is absorbed at matrix–fibre boundaries

300

The strong component of a composite that provides most of the tensile strength

Reinforcement (fibres)

300

Why composites are often anisotropic

Their properties depend on fibre direction

300

A composite where particles, not fibres, provide reinforcement

Particle-reinforced composite

300

Why composites are used in wind turbine blades

High stiffness, low mass, and fatigue resistance

300

A major disadvantage of composites compared to metals

Brittle failure / high cost / difficult repair (any one)

400

A composite made by embedding fibres within a matrix material

Fibre-reinforced composite

400

What happens to a composite’s strength if fibres are poorly bonded to the matrix

Reduced strength due to fibre pull-out / inefficient load transfer

400

A composite commonly used in construction where steel improves tensile strength.

✅ Reinforced concrete

400

A disadvantage that limits composite use in high-temperature environments

Matrix materials soften or degrade at high temperatures

400

Why composites may fail suddenly without plastic deformation

They are brittle and lack a yield region

500

A key reason composites are often preferred over pure metals in engineering applications

High strength-to-weight ratio (also acceptable: corrosion resistance)

500

Why fibre length affects the effectiveness of reinforcement

Fibres must exceed a critical length to transfer stress effectively

500

The composite commonly used in aircraft wings due to its high strength-to-weight ratio

Carbon fibre reinforced polymer (CFRP)

500

Why composites are harder to recycle than metals

They consist of bonded different materials that are difficult to separate

500

The main safety concern when composites fail in structural applications

Sudden catastrophic failure with little warning