Lecture notes on fatigue, static tensile strength and stress corrosion of aircraft materials and structures: Part I: text

The stress intensity factor of small cracks at notches

Fatigue crack growth in 7475-T7651 material under flight-simulation loading. Information from a Douglas report

A new fatigue resistant material: Aramide Reinforced Aluminium Laminate (ARALL)

Differences between the growth of small and large fatigue cracks. The relation to threshold K-values

The effect of blunt notches and saw cuts on the static strength of 2024-T3 and 7075-T6 sheet material

Prediction of fatigue crack growth in 2024-T3 Alclad sheet specimens under flight-simulation loading. Results from a Garteur program

The effect of an irregular crack front on fatigue crack growth

Stress gradients around notches

Trouble shooting in aeronautics and the usefulness of microscopes

Some formulas for the crack opening stress level

Prediction methods for fatigue crack growth in aircraft material

Shear lips on fatigue fractures in aluminium alloy sheet material

Tongue-shaped crack extension during fatigue of high strength aluminium alloys

Environmental effects on fatigue fracture mode transitions observed in aluminium alloys

Four lectures on fatigue crack growth

Fatigue properties of adhesive-bonded laminated sheet material of aluminum alloys

Fatigue crack growth in lugs and the stress intensity factor

Statistical transformation of load histories applied in flight-simulation tests

Internal fatigue cracks are growing in vacuum