de Vries, Various parameters concerning the residual strength of aircraft materials, Master Thesis, Delft University of Technology, 1994 [3] Tjerk J

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Bibliografia

[1] Tjerk J. de Vries, Blunt and sharp notch behaviour of Glare laminates, Delft University of Technology, 2001

[2] Tjerk J. de Vries, Various parameters concerning the residual strength of aircraft materials, Master Thesis, Delft University of Technology, 1994 [3] Tjerk J. de Vries, Marco Pacchione, The Application of the R- curve Concept for the Prediction of the Residual Strenght of Fiber Metal Laminates, Delft University of Technology, 1997

[4] Ad Vlot e Jan Willem Gunnink, Fiber Metal Laminates An introduction, Delft University of Technology, 2001

[5] Jalving, N.H., Health, Safety and Enviromental Aspects of tha mani- facturing and processing of Glare, report B2v-00-02, Delft University of Technology, 2000

[6] Bresser and Dietrich, On the Residual Strength of Glare CCT Specimen with Saw Cuts, Impact and Fatigue Cracks, TN-DA-94-104, Deutsche Aerospace Airbus, Germany, 1994

[7] Bresser D., Survey on the method for determination of the Residual Strength of Fibre Metal Laminates, TN-0047/95, Deutsche Aerospace Airbus, Germany, 1995

[8] ASTM-E561-98, Standard Practice for R-Curve determination, An- nual book of ASTM standards, Metal tests method and Analytical procedures

[9] Sutton G.R., The damage tolerance of fibre reinforced aluminium al- loy laminates, DRA/SMC/CR962001, Defence Research Agency, United Kingdom, 1996

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[10] C.A.J.R. Vermeeren, Residual Strength Prediction for fibre metal laminates: The R-Curve approach, Report LR-717, Delft University of Technology, 1993

[11] T. Testi, A Study on the compliance calibration for Glare, Master Thesis, Politecnico di Milano, Italy, 1995