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Fracture, Toughness and Strength by Gordon Williams

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Introduction Strength is not a material property For ductile materials we have flow and necking For brittle materials we have failure from flaws Surface polishing, a transition from brittle to ductile Griffith ideas

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Griffith(1922) All bodies contain flaws Fracture is from these flaws Used “Energy Release Rate” (see later) Defined as “G” G>G c, energy per unit of created surface area (J/m^2) G c is a basic material property

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Fig 1 W 2a2a H b

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Griffith at fracture In general, Y 2 is a geometric factor, Y 2 = for an infinite plate To find G c vary a, measure , calculate Y 2 hence EG c From E find G c

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Griffith From E find G c If only stresses needed use K c G c preferred, better physics The strength problem “ a ” exists, flaws, hence is determined

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Compliance Method (Composites) F dd F+dF F o C C( a +d a ) b F ada

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Initial Energy: Work done on a a+da, Final Energy: Change in energy=U 1 +U 2 -U 3 (Shaded area) ie Compliance Method (Composites)

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Compliance: Hence Energy release rate Compliance Method (Composites)

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Energy form:

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Used in impact For DCB F a b hh

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Experimental Method i)Measure C( a ) ii)Measure F at fracture G c iii)True for any form

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Compliance Method From Griffith Solution in General

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Plasticity and Size Effects Basic method is elastic (LEFM) All cracks have a local plastic/damage zone Let c be the zone stress rr a r xx

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Plasticity and Size Effects Local stresses,(singular) » (const., 2 can change) r makes response non-linear, Must be within limits, e.g F 5%, F max

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G c & K c are dependent on Constraint Lowest values are for Plane strain, z =0 in the plastic zone, i.e. lateral constraint. Highest values are for Plane stress, z =0 Plasticity and Size Effects

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z rbrb b Plane stress Plane strain bcbc KcKc

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Plasticity and Size Effects For b >> r z plane strain For b ≈ r z =0, plane stress Transition: b**
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1 ASTM : American Society of Testing and Materials.

1 ASTM : American Society of Testing and Materials.

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