1. Glare: history of the development of a new aircraft material;Vlot,2002
2. Roebroeks G. Towards Glare—the development of a fatigue insensitive and damage tolerant aircraft material, Ph.D. Thesis, Delft University of Technology, Delft, 1991.
3. Beumler Th. Flying Glare®—a contribution to aircraft certification issues on strengths properties in non-damaged and fatigue damaged Glare® structures, Ph.D. Thesis, Delft University of Technology, Delft, 2004.
4. Toi R. An empirical crack growth model for fiber/metal laminates. In: 18th Symposium of the International Committee on Aeronautical Fatigue, Melbourne, Australia, 1995.
5. Fatigue crack growth properties of a Glare3-5/4 fiber/metal laminate;Takamatsu;Engng Fract Mech,1999