6 Flashcards

1
Q

What does a notch do to stress?

A
  • Increase average stress by reducing x-section
  • Concentrates Stress (Kt)
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2
Q

What is Nominal Stress?

A

The average stress in the net-section higher that the applied stress

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3
Q

Stress Concentration factor, Kt=

A

σpeaknominal

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4
Q

For a circular hole, Kt=

A

3

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5
Q

For an elliptical hole, Kt=

A

1+2(a/r)½

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6
Q

What is Fracture Mechanics?

A

The general analysis of the failure of structural materials with existing flaws. The main outcome is fracture toughness

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7
Q

Why is there such a variation between theoretical and experimental bond strength?

A

Stress concentration at microscopic flaws. It is amplified at tips of microscratches, voids, notches, surface scratches, corners etc.

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8
Q

What are Stress Raisers?

A
  • Microcracks
  • Voids
  • Notches
  • Surface Scratches
  • Corners
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9
Q

What does the magnitude of ampification of Stress depend on?

A

Microcrack orientation, geometry and dimensions

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10
Q

Define Fracture toughness?

A

Critical value of stress intensity factor at a crack-tip necessary to produce catastrophic failure under simple uniaxial load

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11
Q

Stress Intensity Factor, KI=

A

fσ(πa)½

a= crack length

KI is a variable

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12
Q

Fracture Toughness, KIC=

A

max(πamax)½

This is a property and increases with refinement of grain size

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13
Q

Design Criterion for KIC

A

KI <=KIC

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14
Q

Brittle materials have

A

Low KIC

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15
Q

KIC decreases when

A
  • Strain rate increases
  • Temperature decreases
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16
Q

KIC increases when

A

Grain size decreases

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17
Q

Cracks will suddenly grow if

A

Load is too high, leading to fracture in a brittle manner

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18
Q

Ductile fracture occurs in a

A

Transgranular manner- Through the grains

19
Q

Brittle fracture occurs in a

A

Intergranular manner- along grain boundaries. Enhanced by impurities

20
Q

How does ductile fracture occur in a simple tensile test?

A
  1. Nucleation, growth and coalescence of microvoids at necked region
  2. The stress then causes seperation of grain boundaries
  3. As local stress increases, microvoids grow and coalesce into larger cavities
  4. Eventually metal-metal contact is too small to support load thus fracture
21
Q

Which is more notch-sensitive under tensile loading; Brittle or Ductile?

A

Brittle

22
Q

What is Fatigue?

A

The lowering of strength or failure of a material due to repetitive stress

23
Q

What are the 3 stages of fatigue?

A
  1. A small crack nucleates at the surface and can include scratches, pits, sharp corners, inclusions, grain boundaries or dislocation concentrations
  2. Crack gradually propagates as the load continues to cycle
  3. Sudden fracture when remaining x-section is too small to support applied load
24
Q

For Fatigue to occurs at least part of the load must be

A

Tensile

25
Q

Fatigue is common in

A

Plastics and metals. Not common in ceramics due to low fracture toughness

26
Q

What is Striation?

A

The cyclic build up of crack growth from a surface intrusion. These are on a finer scale and show the position of crack tips after each cycle

27
Q

What is Granular portion of Fracture surface?

A

Rapid crack propagtion at the time of catastrophic failure

28
Q

How are the theoretical infinite stresses relieved at tip ends in practice ?

A
  • Ductile materials- Blunted crack tips
  • Some polymers- Elongated voids with bridging structure
  • Brittle materials- regions of high density tiny cracks
29
Q

What is thermal fatigue?

A

Repeated heating and cooling can cause cyclic stresses due to differential thermal expansion and contraction

30
Q

Mean Stress, σmean=

A

(σmax+σmin)/2

31
Q

Stress amplitude, σa=

A

maxmin)/2

32
Q

Stress range, σr=

A

σmaxmin

33
Q

Stress ratio, R=

A

σminmax

34
Q

Stress concentration decreases the

A

Fatigue limit

35
Q

Low cycle fatigue

A

High loads, plastic and elastic deformation

36
Q

High cycle fatigue

A

Low loads, elastic deformation

37
Q

Define fatigue limit

A

When the S-N curve becomes flat when stress amplitude decreases to a certain level

38
Q

What is fatigue strength?

A

For materials that don’t show fatigue limit, the stress level at which the failure will occur for a specified nuber of cycles

39
Q

Endurance Ratio=

A

Fatigue limit/Tensile Strength ≈ 0.25-0.5

40
Q

Factors affecting Fatigue Life?

A
  • Magnitude of stress
  • Qualities of surface
  • Thermal fatigue
  • Corrosion fatigue
41
Q

Ways to improve fatigue life

A
  • Polishing
  • Introducing compressive stress by “shot peening”
  • Case hardening- Introduces compressive stress
  • Optimize geometry- no internal corners etc.
42
Q

Stress intensity factor, delta K=

A

f(σmaxmin)(πa)½

43
Q

Selection criteria for fatigue?

A
  • Initiation and growth of small cracks= 80-90% of total life. Remainder of life has fast groth to failure
  • Experimental strength justification based on S-N fatigue (safe life)
  • Experimental life 3-4 times required life
  • Thickness of fatigue critical parts is greater than required for static strength
44
Q

Means to increase life?

A
  • Damage tolerance approach
  • Avoid stress concentrations
  • Less fatigue senstive materials