Goodman relation explained

Within the branch of materials science known as material failure theory, the Goodman relation (also called a Goodman diagram, a Goodman-Haigh diagram, a Haigh diagram or a Haigh-Soderberg diagram) is an equation used to quantify the interaction of mean and alternating stresses on the fatigue life of a material.[1] The equation is typically presented as a linear curve of mean stress vs. alternating stress that provides the maximum number of alternating stress cycles a material will withstand before failing from fatigue.[2] [3]

A scatterplot of experimental data shown on an amplitude versus mean stress plot can often be approximated by a parabola known as the Gerber line, which can in turn be (conservatively) approximated by a straight line called the Goodman line.[4]

Mathematical description

The relations can be represented mathematically as:

(n\sigmam
\sigmab

)2+

n\sigmaa
\sigmaw

=1

, Gerber Line (parabola)
\sigmam
\sigmab

+

\sigmaa
\sigmaw

=

1
{n
}, Goodman Line
\sigmam
\sigmay

+

\sigmaa
\sigmaw

=

1
{n
}, Soderberg Line

where

\sigmaa

is the stress amplitude,

\sigmam

is the mean stress,

\sigmaw

is the fatigue limit for completely reversed loading,

\sigmab

is the ultimate tensile strength of the material and

n

is the factor of safety.

The Gerber parabola is indication of the region just beneath the failure points during experiment.

The Goodman line connects

\sigmab

on the abscissa and

\sigmaw

on the ordinate. The Goodman line is much safer consideration than the Gerber parabola because it is completely inside the Gerber parabola and excludes some of area which is nearby to failure region.

The Soderberg Line connects

\sigmay

on the abscissa and

\sigmaw

on the ordinate, which is more conservative consideration and much safer.

\sigmay

is the yield strength of the material.[5] [6]

The general trend given by the Goodman relation is one of decreasing fatigue life with increasing mean stress for a given level of alternating stress. The relation can be plotted to determine the safe cyclic loading of a part; if the coordinate given by the mean stress and the alternating stress lies under the curve given by the relation, then the part will survive. If the coordinate is above the curve, then the part will fail for the given stress parameters.[7]

References

Bibliography

Further reading

External links

Notes and References

  1. Tapany Udomphol. "Fatigue of metals" . 2007.
  2. Herbert J. Sutherland and John F. Mandell. "Optimized Goodman diagram for the analysis of fiberglass composites used in wind turbine blades".
  3. David Roylance. "Fatigue". . 2001.
  4. https://wayback.archive-it.org/all/20120905140833/http://www.eng.auburn.edu/users/marghitu/chapter3.pdf "Fatigue"
  5. Book: Bhandari, V. B.. Design of Machine Elements. Tata McGraw-Hill Education. 2007. 9780070611412. 184, 185.
  6. Book: Shigley's Mechanical Engineering Design. The Mc-Graw-Hill Companies. 2011. 9780073529288. 305.
  7. Hertzberg, pp. 530-31.