1. Development of fibre metal laminates for advanced aerospace structures;Vogelesang;J Mater Process Technol,2000
2. Marissen R. Fatigue crack growth in ARALL – a hybrid aluminium–aramid composite material. Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt e.V. (DFVLR); 1989.
3. Roebroeks GHJJ. Towards GLARE – the development of a fatigue insensitive and damage tolerant aircraft material. PhD thesis, Delft University of Technology; 1991.
4. De Vries TJ. Blunt and sharp notch behaviour of Glare laminates. PhD thesis, Delft University of Technology; 2001.
5. Verolme K. The development of a design tool for fibre metal laminate compression panels. PhD thesis, Delft University of Technology; 1995.