Unit 5 - Fatigue Flashcards

1
Q

What are the characteristics of fatigue failures?

A

Occur without obvious warning, resulting in a brittle appearing fracture.
No gross deformation at fracture.
Macroscopic fracture surface usually normal to principal tensile stress.

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2
Q

How is a fatigue failure recognised and what are its stages?

A

Recognised by smooth region (crack propagation) and rough region (ductile failure).
Three stages: 1) Initiation, 2) Fatigue Crack Growth (two distinct stages), 3) Overload/Failure.

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3
Q

What factors are necessary to cause fatigue failure?

A

(1) Maximum tensile stress of high value.
(2) Large variation/fluctuation in applied stress.
(3) Large number of cycles of the applied stress.

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4
Q

What are the predominant control modes for a fatigue test?

A

Load controlled (Loading profile constant, Compliance varies).
Strain (or extension) controlled (Compliance constant, Loading profile varies).

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5
Q

What types of fatigue tests are there?

A

SN – Counting cycles to failure at given stress/strain.
Fatigue crack growth – Variability in FCG rate across materials/environments.
Notched fatigue performance - Effect of Kt on fatigue life.
Threshold tests – Lowest stress intensity for crack growth.

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6
Q

What is the S-N curve and its significance?

A

Shows stress (S) vs. number of cycles (N) to fatigue failure.
Log scale for N, various stress values plotted.
Low Cycle Fatigue (LCF < 10^6 cycles), High Cycle Fatigue (HCF > 10^6 cycles), Very High Cycle Fatigue (VHCF > 10^9 cycles).

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7
Q

How is an S-N curve determined?

A

Test first specimen at high stress for short-cycle failure.
Decrease stress for each specimen until run out (no failure) in specified cycles.
Fatigue limit is the highest stress with run out.

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8
Q

What are the structural features of fatigue?

A

Crack initiation – Early development, removable by thermal anneal.
Slip-band crack growth – Stage I, deepening crack on high shear stress planes.
Crack growth on high tensile stress planes – Stage II, normal to maximum tensile stress.
Ultimate ductile failure – Occurs when crack length exceeds load-bearing capacity.

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9
Q

What are the key conclusions about fatigue loading cycles?

A

Defined through waveforms (sine, triangular, square, trapezoidal).
LCF characterized by gross plastic deformation, HCF by elastic behavior.
No definitive endurance stress; fatigue limit varies.
Mean stress effects characterized through the Goodman diagram.
Cyclic Stress Strain Curve (CSSC) represents material response to cyclic loading, not monotonic stress/strain.

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