Print Email Facebook Twitter The effect of the sheet width on the fatigue crack propagation in 2024-T3 Alclad material Title The effect of the sheet width on the fatigue crack propagation in 2024-T3 Alclad material Author Schijve, J. Nederveen, A. Jacobs, F.A. Institution National Aerospace Laboratory NLR Date 1965-03-31 Abstract The size effect on crack propagation was studied with sheet specimens of 2024-T3 Alclad. Values of the width were 80, 160, 300 and 600 mm, sheet thickness 3 mm, mean stress 8 kg/mm2 and stress amplitudes 2.5, 4 and 6.5 kg/mm2. Results are compared with the theory of the stress intensity factor and the Weibull theory. Practical implications of the results are indicated To reference this document use: http://resolver.tudelft.nl/uuid:7e5c5102-a4d0-4269-b196-01a52fa13b8b Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR-TR M.2142 Part of collection Aerospace Engineering Reports Document type report Rights (c)1965 National Aerospace Laboratory NLR Files PDF NLR-TR.M.2142.pdf 15.53 MB Close viewer /islandora/object/uuid:7e5c5102-a4d0-4269-b196-01a52fa13b8b/datastream/OBJ/view