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Now showing items 11-20 of 20

The influence of testing parameters on stress corrosion crack growth in the high strength aluminium alloy 7010-T651

Schra, L. (National Aerospace Laboratory NLR, 1996)

Fatigue and fracture in an aircraft engine pylon

Wanhill, R.J.H.; Oldersma, A. (National Aerospace Laboratory NLR, 1996)

Gust load conditions for fatigue tests based on a continuous gust concept

Jonge, J.B. de; Vink, W.J. (National Aerospace Laboratory NLR, 1997)

Impact damage and failure mechanisms in structure relevant composite specimens

Wiggenraad, J.F.M.; Ubels, L.C. (National Aerospace Laboratory NLR, 1997)

Residual strength tests of stiffened panels with multiple site damage

Hoeve, H.J. ten; Ottens, H.H.; Schra, L.; Vlieger, H. (National Aerospace Laboratory NLR, 1998)

The influence of stitching fibre and stitching density on the failure strains of CFRP fabrics

Thuis, H.G.S.J.; Herzberg, I.; Loh, A.; Bannister, M.K. (National Aerospace Laboratory NLR, 1998)

Impact damage prediction and failure analysis of heavy loaded, blade- stiffened composite wing panels

Wiggenraad, J.F.M.; Zuang, X.; Davies, G.A.O. (National Aerospace Laboratory NLR, 1998)

Failure criterion for the skin-stiffener interface in composite aircraft panels

Rijn, J.C.F.N. van (National Aerospace Laboratory NLR, 1998)

Review of aeronautical fatigue investigations in the Netherlands during the period March 1997 - March 1999

Ottens, H.H. (National Aerospace Laboratory NLR, 1999)

Corrosion and fatigue assessment of aircraft pressure cabin longitudinal lap splices

Wanhill, R.J.H. (National Aerospace Laboratory NLR, 1999)

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