Abstract
Abstract
A method to determine the plane stress fracture resistance curve for the stable crack growth of ductile material is presented. A reinforced double cantilever beam (RDCB) specimen of thin grooved section is used to determine the COD and JR of aluminium 2024-T3 material which exhibits substantial stable crack growth. The method makes use of the BEF and Dugdale models to determine the load-deflection behaviour of the specimen. The derivation is based on the experimentally determined load and crack extension values.
The crack growth resistance for specimens of different thicknesses are deduced using the proposed method and are compared with those of the compliance method as well as the finite element method.
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