Fracture II Flashcards

1
Q

What does fatigue occur in?

A

Fatigue occurs in structures subject to dynamic and varying stress – metals,
composites, ceramics, plastics…

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2
Q

When does fatigue occur?

A
  • Occurs after a long time of cyclic stress
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3
Q

What stress levels can fatigue occur at?

A

Failure at stress levels below yield or tensile strength of the material due to imperfections

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4
Q

What are the three stages of fatigue?

A
  • Initiation
  • Propagation
  • Final fracture (K=Kc)
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5
Q

What can be defined from a S-N curve?

A

Fatigue strength and fatigue life can be defined from an S-N curve

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6
Q

What is the fatigue limit?

A

the stress amplitude at which fatigue
failure does not occur; it is exhibited at low stress amplitudes in some
materials (eg. steel) but not others

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7
Q

What do cyclic stresses cause that leads to fatigue?

A

crack nucleation and growth and crack propagation, leading to fatigue fracture.

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8
Q

What are methods that improve fatigue life/reduce fatigue failure?:

A
  1. Shot-Peening
  2. Case hardening
  3. Mechanical Design (reducing sharp concerns)
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9
Q

What can stress concentrations arise from( i.e. sources of stress concentration) ?

A
  • mechanical surface
    damage
  • residual stress from
    manufacturing
  • corrosion pitting
  • sharp corners (design)
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10
Q

What happens during shot-peening?

A
  • Residual compressive
    stresses are generated
    on the surface of a
    metal by shooting hard
    particles at it
  • Residual compressive
    stresses delay crack
    initiation (may retard
    crack growth)
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11
Q

What happens during case hardening?

A
  • Hardens the surface of a metal object
    while allowing the metal underneath
    to remain tough (high Kc)
  • A carbon- or nitrogen-rich surface
    layer is created through atomic
    diffusion by exposing the metal to a
    carbon or nitrogen rich atmosphere at
    a high temperature
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12
Q

What types of cyclic loading are imposed on
components of a jet-engine?

A
  1. Temperature cycles (engine start-up)
  2. Loading cycles (take off, cruise, landing)
  3. Blade flutter and vibrations (rotation)
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13
Q

When do cracks usually nucleate?

A

*Cracks usually nucleate in the first 10-20% of
service life

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14
Q

Why is there a range in the probability of fatigue failure?

A

There is variability in number and distribution of defects
within a component due to processing

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15
Q

What is the relationship between mean stress and fatigue life?

A

increasing the mean stress
level leads to a decrease in fatigue life.

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16
Q

Name the factors that affect fatigue life:

A

Mean Stress, Stress Amplitude, Surface Treatment, and Mechanical Design

17
Q

How can fatigue life be improved with mechanical design? Provide an example covered in class.

A

By incorporating
rounded fillet into a rotating shaft where there is a change in diameter.

18
Q

How do sharp corners impact fatigue failure?

A

Sharp corners are stress raisers, and can render the component
more susceptible to fatigue failure

19
Q

Where are beach marks found?

A

Found where crack propagation occurred

20
Q

What is beachmark spacing indicative of?

A

The rate of crack propagation

21
Q

What is the single largest cause of failure?

A

Fatigue failure

22
Q

Where do cracks start for fatigue failure?

A

Cracks start at stress concentration points, usually
on surface – dents, scratches, sharp fillets, keyways, machined threads etc

23
Q

What is the length at which fatigue failure occurs?

A
  • Failure occurs when crack grows to critical length –
    ie. when Kc is exceeded
24
Q

What type of stress is needed for crack nucleation and growth and why?

A

Tensile stress required – cracks will not form if there are
only compressive stresses present

25
Where can cracks nucleate for fatigue failure?
Cracks can nucleate internally on microstructure discontinuities (eg. porosity, inclusions etc.) or on the surface –dents, scratches, sharp fillets, key-ways, machined threads etc.
26
Why is significant time important for initiation and crack growth?
* This way, cracks can be found by inspection of structures: This is why we design structures with critical crack lengths that are large and easily detectable.
27
What is the difficulty with internal fatigue cracks?
Internal fatigue cracks can be a lot more difficult to detect
28
What are beachmarks?
Macro-scale features usually associated with the periodic start-up of machinery; they do not reflect load cycles, but indicate rate of crack propagation
29
What are striations?
Micro-scale features indicating crack origin and growth characteristics; indicative of load cycles
30
What are the physical features of fatigue failure?
Beachmarks and striations.
31
What is the relationship between mean stress and fatigue life?
Increasing the mean stress level leads to a decrease in fatigue life.
32
How can striations be observed?
Using electron microscopy
33
What do beachmarks result from?
Interruptions in the stress cycles.
34
What does each fatigue striation correspond to?
The advance of a fatigue crack during a single load cycle.