Fatigue Overview Flashcards

1
Q

What is fatigue the process of?

A

Repeated vibrations in loading causing failure even when the nominal stresses are below the material yield strength

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

What is fatigue made up of?

A

Crack initiation and subsequent crack growth as a result of cyclic, plastic deformation

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

What is deltasigma?

A

= sigma(max) - sigma(min)
Change in stress

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

What is sigma(m)?

A

(sigma(max)+sigma(min))/2
Mean stress

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

What is sigma(a)?

A

Stress amplitude
deltasigma/2

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

What can cause crack initiation for a fatigue crack from a smooth surface?

A

Slip in grains

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

What can cause crack initiation in a notched surface for a fatigue crack?

A

High concentrations of strain at the root of the notch, with possible fracture of inclusions

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

What is the scale of short crack growth?

A

The scale of the mircostructure

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

What is stable crack growth?

A

‘Long’ cracks in the body of a metal growing regularly as the stress cycles

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

What is ‘end of life’ for a fatigue crack?

A

Rapid bursts of crack growth under massive plastic strain or brittle failure

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

What is the difference between elastic and plastic deformation in reference to bonds?

A

Elastic = stretching bonds
Plastic = breaking & reforming bonds

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

How can slip planes contribute towards crack initiation?

A

They essentially form a notch when they slip due to the application of a tensile stress

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

What are some other initiation triggers?

A

-Cracking / debonding of second phase particles
-Scratches / machining marks on surface
-corrosion pits or intergranular attack
-Porosity from casting
-Brittle surface layers

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

What are the common stages of a crack growing under a tensile stress?

A

Stage I: Shear crack
Stage II: Tensile crack

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

What is the process of growth for a tensile crack?

A

As stress increases, the crack opens
Shear stresses at the tip grow
The crack is opened and blunted
As stresses fall, the crack closes
It has grown by a very small amount

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

What is safe life?

A

Evaluate expected life
Use a margin of safety
Design to survive expected service life
Retire

17
Q

What is fail safe?

A

Provides redundant load paths
Design to fail into a safe condition then survive until repair

18
Q

What is deflect tolerance?

A

Assume flaws do exist
Design to live with some crack growth below critical size
Requires regular inspections

19
Q

What is S-N?

A

The Total Life method
Relates nominal or local elastic stress to total life

20
Q

What is epsilon-N?

A

Crack Initiation (or Strain-Life) method
Relates local strain to crack initiation life

21
Q

What is LEFM?

A

Crack Propagation method
Relates stress intensity to crack propagation rate

22
Q

What do S-N, epsilon-N and LEFM have in common?

A

They all rely on similitude

23
Q

What does N(f) = N(i) + N(p) mean?

A

Total life = crack initiation + crack growth

24
Q

State the Paris equation

A

da/dN = C(deltaKI)^m

25
Q

What is da/dN?

A

Crack growth rate

26
Q

What can KI be replaced by?

A

Ydeltasigmasqrt(pi*a)

27
Q

What is needed to calculate lifetimes?

A

Initial crack size
Final crack size
Stress range
K calibration
Material growth law

28
Q

What are some limitations for designing against fatigue?

A

Life calculations are less precise than strength calculations
Fatigue properties cannot be inferred from static mechanical properties
Lab tests often exhibit scatter and are difficult to translate to full-sized components