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116

a) Radial crack in disk

b) Disk cracked longitudinally

Figure 11: Radial (a) and longitudinal (b) cracks in a disk

Figure 12: Stress profile through the thickness determined by finite element analysis /12/

Membrane and bending stress components are calculated from the principal stresses

normal stresses,

σ

1

and

σ

2

:

Membrane stress component

Bending stress component

(

)

1 2

1

2

m

σ

σ

σ

= +

(

)

1 2

1

2

b

σ

σ

σ

= −

If the cross section contains a crack, the secondary stresses can be a major loading

component (typical secondary stresses are welding residual stresses). Secondary stresses

are taken into account in determining the K factor, but not in determining the limit load,

FY, or the degree of ligament plasticity, Lr.