Composite Materials for Aircraft Structures, Second Edition

The advantages and disadvantages of forming joints by adhesive bonding and bolting or riveting are summarized in Table 9.1
| Advantages | Disadvantages |
|---|---|
| Bonded Joints | |
| Small stress concentration in adherends | Limits to thickness that can be joined with simple joint configuration |
| Bolted Joints | |
| Positive connection, low initial risk | Considerable stress concentration |
Although there are many advantages for bonding composites from the performance view point, there are also many limitations or disadvantages that must be considered with each potential application. For a relatively thin-skinned structure, particularly where fatigue may be a problem, bonding is very attractive indeed. However, the use of suitable pre-bonding surface...