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Fatigue initiation and crack growth behaviour in GLARE from the Airbus MegaLiner Barrel test
(National Aerospace Laboratory NLR, 2006)
GLARE teardowns from the MegaLiner Barrel (MLB) fatigue test
(National Aerospace Laboratory NLR, 2009)
Fatigue and Damage Tolerance Evaluation of Structures: The Composite Materials Response
(National Aerospace Laboratory NLR, 2009)
A New Fibre Placement Architecture for Improved Damage Tolerance
(National Aerospace Laboratory NLR, 2010)
Interlaminar shear strength criteria for composites
(National Aerospace Laboratory NLR, 2009)
Design optimization of stiffened composite panels for damage resistance
(National Aerospace Laboratory NLR, 2000)
Design guidelines for the prevention of skin-stiffener debonding in composite aircraft panels
(National Aerospace Laboratory NLR, 2000)
Design and analysis of stiffened composite panels for damage resistance and tolerance
(National Aerospace Laboratory NLR, 2002)