Failure Analaysis

   Failure as a Design      Criterion

   Fracture Mechanics

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Tutorial Questions

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Griffith Equation


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Stress Intensity Factor and Fracture Toughness Testing
- Stresses Close to a Crack Tip
- Fracture of Glass
- High Strength Versus high Toughness
- Quenching and Residual Stress
- Missile Motor Case Fracture
- Fracture Toughness Tests
- Plastic Zone Effect
- Specimen Thickness Effect
- Growth of Semi-Elliptic Flaws
- Leak-Before-Break Concept
- Pressurised Vessels
- Fracture of a Beer Barrel
- Pin-Loaded Lug
- Materials Selection and Temperature
- Chemical Reactor Vessel
- Fracture of Ice


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Characterising Sub-Critical Growth
 -  Fatigue Life Prediction
 -  Stress Corrosion Cracking

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Theory Resource



Problem 9

This question is designed to demonstrate why one uses the semi-minor axis to assess the criticality of surface defects and to indicate that cracks tend towards a stable aspect ratio (2c/a). It requires some thought in interpreting the table of geometry correction factors but is straightforward and should take about 10 minutes to complete.

A thin leaf spring experiences unidirectional bending and develops a semi-elliptic crack on the tensile surface. The crack has an initial aspect ratio of 0.2 when found. The plane of the crack is perpendicular to the direction of applied bending stress. As the spring undergoes repeated deflection, the crack grows by fatigue.

Using the K solution and geometry correction factors for tensile loading, given in the table below, determine whether the ellipticity ratio of the crack will increase or decrease. The figure below shows the crack geometry.

wpe1.jpg (7725 bytes)

a/c

Phi

Y

a/B

0.2

0.4

0.6

0.8

1.051

0.2

0o

45o

90o

0.617

0.990

1.173

0.724

1.122

1.359

0.899

1.384

1.642

1.190

1.657

1.851

1.151

0.4

0o

45o

90o

0.767

0.998

1.138

0.896

1.075

1.225

1.080

1.247

1.370

1.318

1.374

1.447

1.277

0.6

0o

45o

90o

0.916

1.024

1.110

1.015

1.062

1.145

1.172

1.182

1.230

1.353

1.243

1.264

1.571

1.0

0o

45o

90o

1.174

1.067

1.049

1.229

1.104

1.062

1.355

1.181

1.107

1.464

1.193

1.112



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