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presentation displays mean stress effects in the safe-life, infinite-life regime, proposed by

Haigh. The Haigh diagram is a plot of real data, but it requires an enormous amount of

information. More convenient means to show the same information incorporates the

Haigh diagram with

S

max

and

S

min

axes to produce a constant-life diagram (Fig. 3).

10

3

10

4

10

5

10

6

10

7

10

8

0

100

200

300

400

500

600

700

800

Steel

Nonferrous

Stress amplitude,

Δ

S/2, MPa

Number of cycles failure

Figure 1: Schematic

S

-

N

representation of materials having asymptotic fatigue limit behaviour

(up) and those displaying a fatigue strength response - continuously decreasing property (down)

10

4

10

5

10

6

10

7

0

100

200

300

400

500

600

700

800

a

)

R = -1

R = 0

R = 0.6

Stress amplitude,

Δ

S/2, MPa

Number of cycles to failure

10

4

10

5

10

6

10

7

0

40

80

120

160

200

b

)

R = 0.6

R = 0

R = -1

Maximum stress, MPa

Number of cycles to failure

Figure 2: The influence of method of

S

-

N

data presentation on the effect of

R

(=

S

min

/

S

max

) value.

Stress amplitude

S

a

vs. number of cycles

N

(left), maximum stress

S

max

vs. N (right) /10/

For general consideration of mean stress effects, various models of the mean-ampli-

tude response have been proposed. A commonly used presentation is the Goodman line,

although other models are possible (e.g., Gerber and Soderberg). The conventional plot

associated with this problem is produced using the Haigh diagram, with the Goodman

line connecting the ultimate strength on

S

max

, and the fatigue limit, corrected fatigue limit,

or fatigue strength, on

S

a

. This line then defines the boundary of combined mean-

amplitude pairs for anticipated safe-life response. The Goodman relation is linear and can

be readily adapted to a variety of manipulations.

In many cases Haigh or constant-life diagrams are simply designed, using the

Goodman presentation approximating actual response through the model of the beha-

viour. For materials that do not have a fatigue limit, the fatigue strength at a given