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Corrosion Fatigue
Corrosion fatigue is a special
case of stress corrosion caused by the combined effects of cyclic stress
and corrosion. No metal is immune from some reduction of its resistance
to cyclic stressing if the metal is in a corrosive environment. Damage
from corrosion fatigue is greater than the sum of the damage from both
cyclic stresses and corrosion. Control of corrosion fatigue can be
accomplished by either lowering the cyclic stresses or by corrosion
control.
The "beach
marks" on the propeller shown below mark the progression of fatigue
on this surface.

Similar beach marks are shown
on the aerospace part below left. The high magnification scanning
electron microscope image on the right shows striations (individual
crack progression marks). The part shown below is also discussed in the
section on fretting corrosion.
An infamous example of
corrosion fatigue occured in 1988 on an airliner flying between the
Hawaiian islands. This disaster, which cost one life, prompted the
airlines to look at their airplanes and inspect for corrosion fatigue.

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