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Perhaps the most familiar type of fatigue test would be classified as a "crack initiation" process. With this method, specimens of a material (or the actual parts) are subjected to repeated stress cycles until a crack is initiated . . .or is allowed to continue to grow until total fracture occurs. Stress cycles can be applied axially, in plane bending, in rotating bending, in torsion, or in combination. These test modes utilize cycles of minimum to maximum tensile stress, or reversed cycles of tensile and compressive stress. The resultant of the minimum stress divided by the maximum stress is termed the "stress ratio."


HOW IS A FATIGUE TEST CONDUCTED?

Each test specimen is cycled over a constant load (stress) or displacement (strain) range until a crack or total fracture occurs. The number of test cycles required to produce the desired failure yields a single data point. Multiple specimens are tested at selected stress levels and the number of cycles to failure of each is plotted against the applied stress amplitude. 


HOW ARE RESULTS INTERPRETED?

The widely accepted graphical representation of fatigue data points is the S/N diagram first introduced over a century ago by August Wohler. This method locates the cyclic stress amplitude (S) on the vertical axis and the number of cycles to failure (N) on the horizontal axis. 

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< Typically, a logarithmic scale is used for the horizontal axis while the vertical axis uses a linear scale. Specimens are tested in a series of decreasing stress levels until no failure occurs within a selected maximum number of cycles (usually 10 million cycles). The nearly horizontal portion of the curve defines the fatigue or endurance limit for the test material. For many nonferrous materials, however, there will not be a definite endurance limit and the low stress portion of the curve will not have a horizontal slope. 

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HOW MANY SPECIMENS ARE REQUIRED FOR AN ACCURATE FATIGUE TEST?

The number of specimens necessary to complete an S-N curve... or Goodman diagram... will depend on several factors. The amount of "scatter" in the data and the desired confidence level will often dictate how many samples should be tested. Properly prepared specimens of homogeneous materials may require only about 10 data points to adequately describe an S-N curve. For higher levels of confidence or for materials that exhibit variances in composition, many more specimens may be required to yield a definitive curve.

HOW COULD WE USE THE TEST INFORMATION?

Fatigue data can be used for a number of purposes, including the evaluation of...

Various manufacturing processes.
Different material compositions.
Variances in material lots.
Effects of surface finish, heat treating, shot peening and other geometric factors
Effects of corrosive or high temperature environments.
Optimizing designs.
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Another graphical format is the Goodman diagram, which displays the effect of the test stress ratio. The mean stress is plotted on the horizontal axis against the cyclic or working stress range (minimum to maximum) on the vertical axis. Each data point represents the combined value of the mean stress and the maximum cyclic stress which will yield infinite life, or cause a fatigue failure at a fixed number of cycles. The apex is the point where the mean stress and the maximum cyclic stress both equal the ultimate tensile strength of the material. The Goodman diagram is particularly helpful in determining the effectiveness of a material or component that will be subjected to a cyclic stress superimposed upon a non-zero mean stress. Typical examples of such an application include bolted or riveted joints, vehicle suspension systems, aircraft structures, turbine blades, etc.

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WHAT ARE SOME APPLICATIONS?

Specific examples of applying fatigue test results cover a wide variety of situations:

bullet.GIF (509 bytes) Quality control of piston forgings
bullet.GIF (509 bytes) Effects of laser etching prosthetic devices
bullet.GIF (509 bytes) Integrity of welding processes
bullet.GIF (509 bytes) Evaluating powdered metal materials
bullet.GIF (509 bytes) Durability of electronic circuit connections
bullet.GIF (509 bytes) Compressor valve life expectancy
bullet.GIF (509 bytes) Selection of spur gear alloys
bullet.GIF (509 bytes) Fastener capability comparisons
bullet.GIF (509 bytes) Engine valve treatment analysis
bullet.GIF (509 bytes) Wave spring washer reliability
bullet.GIF (509 bytes) Suspension bridge cable life expectancy
bullet.GIF (509 bytes) Trailer body durability
bullet.GIF (509 bytes) Piston ring quality
bullet.GIF (509 bytes) Effects of plastic bead shot peening
bullet.GIF (509 bytes) Evaluation of casting processes
bullet.GIF (509 bytes) Steel chain quality control

... and MANY MORE.

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