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7/31/2019 12 Fatigue SN Approach Fracture Approach Notes
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Objectives
1. Explain the two approaches tofatigue characterization.
2. Explain the different assumptions
underlying the two approaches.3. Identify the fatigue limit, fatigue
strength, and fatigue life from an
S-N curve4. Identify the three regions of
behavior on a da/dn – delta K
curve.
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The Three Horsemen of Engineering
Fatigue
Corrosion Wear
Durer
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Fatigue
- Cyclic Load/ Strain
- Extended time failure process
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Two Types of Fatigue
High Cycle
- Stress below yield strength
- Macroscopically brittle
- May be very long life
Low Cycle
- Stress exceeds yield strength
- Very few cycles to failure
- Lots of plastic deformation
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Terminology
Mean Stress
Range
Stress Amplitude
“R Value”
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Two Engineering Approaches to Fatigue
1. Assume a flaw free structure
- initiation of flaw dominant
- safety factors to account for flaws
2. Assume presence of flaws of
known type
- fracture mechanics for prediction
- measurement/ monitoring required
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High Cycle Fatigue Process
Local yielding at a defect or in a stressconcentration (filet root, scratch, bend, hole)
Dislocation pile up/ saturation
Crack formation
Crack propagation (relatively little of the life)
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S-N Approach
BCC & HCP Metals
MultipleSpecimens
DifferentStresses
Cycled to Failure
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Fatigue in FCC Alloys (Al)
7075-T6 Aluminum – notched,
constant load amplitude
Hardrath et al, NASA TN D-210
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Effect of Notches & Cold Working
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S-N Approach
Assumes Flaw Free Structures or structures withflaws just like the test specimens.
Implies that most of the life of a structureoccurs during crack INITIATION!
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Fatigue Limit vs. Hardness
Metals Handbook, Vol 1, ASM Int.
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Relation between rotating, bending unnotched fatigue strength and
tensile strength, for alloy ( ) steels and carbon (x) steels
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Limitations of S-N
1. Massive Scatter
2. Initiation and propagation not
separate3. Mechanisms change based on
stress
Low cycle –
plastic deformationHigh cycle – purely elastic deformation
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The FCP Process
1. Sharp Crack – closed
2. Stress opens crack
3. Tip of crack blunts
4. Crack closure/ sharpening
5. Repeat
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The Fatigue Process
1. Sharp Crack – closed
2. Stress opens crack
3. Tip of crack blunts
4. Crack closure/ sharpening
5. Repeat
*Note: Large load = large plastic zone =
large compressive stress = difficult crack
opening on next cycle
** Thus periodic overloads during fatigue
may actually slow the failure process
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Load Order Is Significant
l= low load cycle h = high load cycle
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Effect of Stress Level on FCP Rate
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Effect of constant Delta-K Values
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Monitor Stress Intensity and Crack Speed:
da/dN – Delta K