Chapter 3: Failure Flashcards

1
Q

Mechanical failure

A

Unwanted loss of load carrying capacity of a material caused by fatigue, creep, impact or corrosion

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2
Q

Physical failure causes (3)

A

Improper material choice/processing, inadequate design, misuse

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3
Q

Grain boundaries

A

Narrow region with a higher energy between atoms that doesn’t fit perfectly together

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4
Q

Stress concentration

A

Magnified stresses around discontinuities. Ductile materials fail in a brittle manner when present.

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5
Q

Stress concentration formula

A

σmax = σ + 2σsqrt(a/pt)

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6
Q

Stress intensity factor

A

How fast stress multiplies at a crack

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7
Q

Stress intensity factor formula

A

Kt = σmax/σ = 1+2sqrt(a/pt)

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8
Q

Stress concentrations in ceramics formula

A

σc = sqrt((2Eγ) / (pi*a))

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9
Q

Fracture toughness/critical stress intensity formula

A

Kc = γσsqrt(pi*a)

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10
Q

Charpy testing

A

Hitting a notched specimen with a hammer at different temperatures to determine it’s energy to fracture and tendency to become brittle.

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11
Q

Temperature’s relation to type of fracture

A

Ductile fracture happens at higher temperatures, brittle fracture happens at low temperatures

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12
Q

Fatigue

A

Cracking of materials due to cyclic stress.

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13
Q

Mean stress formula

A

σm = (σmax + σmin)/2

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14
Q

Stress amplitude formula

A

σa = (σmax - σmin)/2

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15
Q

Stress-failure curve relationship

A

Plot of mean stress to number of cycles to failure. As σm increases, the curve shifts down and left.

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16
Q

BCC fatigue limit

A

Defined

17
Q

FCC fatigue limit

A

Undefined

18
Q

Failure surfaces, beachmarks, striations

A

Visible markings where crack propagation stopped long enough for oxidation to occur. Initiated via stress concentrations and progress by stress reversals that cause the crack tip to move forward.

19
Q

Ways to decrease fatigue (3)

A

Lowering the mean stress, altering the surface via compression or polishing, reducing exposure to corrosive environments

20
Q

Paris Law

A

Rate of growth of a crack

21
Q

Paris law formula

A

da/dN = C(ΔK)^m

22
Q

Creep

A

Failure of metal below the yield strength due to slow continuous deformation. Needs time, temperature, stress.

23
Q

Creep Temperature

A

0.33 < T/Tmelt

24
Q

Creep test

A

Constant load used to mesure strain

25
Q

Primary creep

A

Work hardening occurs, decreasing slope and strain rate

26
Q

Secondary creep

A

Work hardening cancelled out by recovery, constant slope and strain

27
Q

Secondary creep formulae

A

dε/dt = Ae^(-Q/RT) = Bσ^7

28
Q

Tertiary creep

A

Failure occurs, slope and strain increase

29
Q

Relationship between creep temperature and stress

A

As temperature increases, stress increases