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    Fatigue initiation and crack growth behaviour in GLARE from the Airbus MegaLiner Barrel test 

    Wanhill, R.J.H.; Hattenberg, T.; Haan, P.H. de (National Aerospace Laboratory NLR, 2006)
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    GLARE teardowns from the MegaLiner Barrel (MLB) fatigue test 

    Wanhill, R.J.H.; Platenkamp, D.J.; Hattenberg, T.; Bosch, A.F.; Haan, P.H. de (National Aerospace Laboratory NLR, 2009)
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    Fatigue and Damage Tolerance Evaluation of Structures: The Composite Materials Response 

    Rouchon, J.; Bos, M.J. (National Aerospace Laboratory NLR, 2009)
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    A New Fibre Placement Architecture for Improved Damage Tolerance 

    Nagelsmit, M.H.; Kassapoglou, C.; Gürdal, Z. (National Aerospace Laboratory NLR, 2010)
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    Interlaminar shear strength criteria for composites 

    Creemers, R.J.C. (National Aerospace Laboratory NLR, 2009)
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    Design optimization of stiffened composite panels for damage resistance 

    Wiggenraad, J.F.M.; Vercammen, R.W.A.; Arendsen, P.; Ubels, L.C. (National Aerospace Laboratory NLR, 2000)
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    Design guidelines for the prevention of skin-stiffener debonding in composite aircraft panels 

    Rijn, J.C.F.N. van (National Aerospace Laboratory NLR, 2000)
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    Design and analysis of stiffened composite panels for damage resistance and tolerance 

    Wiggenraad, J.F.M.; Greenhalg, E.S.; Olsson, R. (National Aerospace Laboratory NLR, 2002)

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    AuthorHaan, P.H. de (2)Hattenberg, T. (2)Wanhill, R.J.H. (2)Wiggenraad, J.F.M. (2)Arendsen, P. (1)Bos, M.J. (1)Bosch, A.F. (1)Creemers, R.J.C. (1)Greenhalg, E.S. (1)Gürdal, Z. (1)... View MoreSubject
    Composite materials (8)
    Structural stability (8)
    ... View MoreDate Issued2009 (3)2000 (2)2002 (1)2006 (1)2010 (1)Has File(s)Yes (8)

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