1. W. ‘tHart and R. Diks, Laboratory tests to simulate APU heating on GLARE3-4/3-.4, NLR, Report NLR-CR-99338, 1999.
2. Glare Application For Primary A3XX Airbus Structure, DaimlerChrysler Aerospace Airbus Document, EMF-723/99, Issue 3, 2000.
3. T.J. de Vries, The residual strength of Glare laminates with foreign object damage, Delft University of Technology, EADS Technology Seminar 2001.
4. M. Hagenbeek, Fatigue and residual strength effect of scratches, Delft University of Technology, Report B2V-00-14, 2000.
5. A. de Koning and L. Schra, Fatigue crack growth of part through the thickness cracks in GLARE3 and GLARE4B coupons, NLR, Report NLR-CR-2000.078, 2000.