Lecture 11 - Toughness and Fatigue Flashcards

1
Q

What does Toughness mean?

A

the materials energy absorption and deformation without failure

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2
Q

Can failure happen before ultimate stresses?

A

Yes, the presence of cracks can modify the local stresses to such an extent that the elastic stress analyses done so carefully by the designers are insufficient!

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3
Q

What happens when the cracks reaches the critical length?

A

it can propagate catastrophically through the structure, even though the gross stress is much less than would normally cause yield or failure in a tensile specimen.

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4
Q

What are the 3 mechanics we study for dynamics of cracks?

A

Start, grow, stop

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5
Q

What kind of loading can produce cracks?

A

Static and dynamic load

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6
Q

What are the 3 fracture analysis used for toughness?

A
  • Griffith analysis
  • stress intensity approach
  • strain energy release rate approach
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7
Q

What is the (mostly) good approximation for brittle materials i.e. diamond, glasses?

A
homogenous 
isotropic
linearly elastic
no crack blunting
isothermal conditions
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8
Q

What is the postulate of The Griffith analysis?

A

a crack will propagate if and only if the energy of the system is thereby decreased.

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9
Q

What is the length of a bulk crack and a surface crack?

A

2c and c

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10
Q

What is Gc? And what does a high value mean?

A

Fracture energy, that it is harder to break.

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11
Q

When can you use The stress intensity factor approach?

A
  • homogeneous isotropic and a relatively few anisotropic materials (composites)
  • states of stress other than the simple uniaxial stress used by Griffith
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12
Q

What are the differences between the Griffith analysis and The stress intensity factor approach?

A

• the crack profile and hence the displacement field near the crack are assumed to be parabolic not elliptic!
• Energy absorption due to plastic deformation at the crack tip is included
(Griffith’s original analysis an elastic behaviour until fracture was assumed)

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13
Q

What can we also call The stress intensity factor approach?

A

fracture toughness

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14
Q

What are the 3 failure modes?

A

I Opening mode
II In-plane shear mode
III Anti plane-shear mode

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15
Q

What are the differences between Plane state of stress and Plane state of strain?

A

Thin sheet and thick sheet

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16
Q

Why is Kc>KIc

A

Thus the probability that a material will fracture is the highest in a plane state of strain

17
Q

What are the most widely used test specimen for fracture mechanics test on plastics?

A

the compact tension (CT) specimen [Pacman]

the single-edge-notch bend (SENB specimen) [3-p bending]

18
Q

What is the rule of thumb about KIC?

A

Rule of thumb: materials having a KIc > approx.10 MPa m1/2 are considered to be tough.

19
Q

What is crashworthiness?

A

ability to maintain a survivable volume for the occupants and alleviate the loads transmitted to the occupants during potentially survivable accident scenarios

20
Q

What are the main toughening mechanism for crashworthiness?

A

geometry, structural arrangements, materials and energy

absorption devices used to dissipate the energy, and the interaction of these variables

21
Q

What is the propagation of a crack along an interface between two constituents is controlled by?

A

The interfacial strain energy release rate, or simply interfacial energy, Gi.

22
Q

What is delamination?

A

Delamination is the act of crack growth between adjacent laminae

23
Q

What can delamination also be called?

A

interlaminar fracture

24
Q

What experiments can you do to examine delamination?

A
  • in mode I: double cantilever beam (DCB) test, where GIc is calculated
  • in mode II: end-notched flexure (ENF) test, where GIIc is calculated
25
Q

What is PD and ID?

A

PD (Primary delamination)

ID (Intralayer delamination)

26
Q

Name some of the toughening mechanisms

A
Interfacial fracture
Crack deflection
Delamination
Fiber fracture (contributes the least)
Frictional sliding during fiber pull-out
matrix contribution to composite toughness