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129

Requirements in this respect are realised by the modification of standard isoparametric

elements in adequate way. Elastic singular behaviour

1 /

r

is presented by the isopara-

metric finite elements (with 8 nodes in 2D and 20 nodes by 3D) if the mean node at

element side is moved in direction of crack tip at quarter position. Additionally, to

consider the plasticity, two corner nodes and mean nodes at crack tip must have identical

position from the beginning (the corresponding element edge collaborates in point, in

which way the element passes from rectangular in triangle – from there the name), but

under loading influence they may, to realistically represent crack blunting, be separated.

Because that these collaborate rectangular elements include

1 /

r

and

r

–1

terms, it is

assumed that they will sufficiently accurate describe the behaviour at crack tip in

combination with the standard description of material law in exponential form.

Accordingly, there are three different kinds of elements for crack tip modelling:

Deformed „quarter-point“ element: by this element elastic singularity

1 /

r

is

accurately described.

Collaborated element (from rectangular to triangle) that posses 3 different nodes at

crack tip. With this element

r

-1

singularity is realised, which corresponds to elastic-

ideal plastic materials.

Element that combines both above changes and in this way includes

1 /

r

and

r

-1

singular terms.

If such elements are used for crack modelling, then a couple of their nodes at crack tip

share the same position. When the model is loaded the elements at tip are deformed and

these nodes starts to separate. This leads to crack blunting and realistic modelling of crack

tip behaviour, as shown in Fig. 4.

Figure 3: Idealization of surface and

embedded cracks

Figure 4: Crack tip simulation with the finite element

method

Using finite element method the evaluation of stress intensity and

J

-integral values for

3D-geometries of structures and cracks becomes possible. Independence on integration

contour is principally only valid for 2D case. By 3D-geometry, as in the case of surface

crack (Fig. 5) the independence is only approximative and the deviation is more

expressed with the growing distance from crack tip.