Mechanical Metallurgy Syllabus
Mechanical Metallurgy
Complete Guide for GATE Metallurgy (MT) - Section 6 (TestUrSelf)
Table of Contents
6.1 Stress and Strain Analysis
Stress and Strain Tensors
Stress Tensor (σij)
Strain Tensor (εij)
Mohr's Circle Representation
Mohr's Circle for 2D stress state
Elasticity, Stiffness and Compliance Tensors
Generalized Hooke's Law
Where Cijkl is the stiffness tensor (4th rank, 81 components)
For Isotropic Materials
Where λ and μ are Lamé constants:
Yield Criteria
Von Mises Criterion
Tresca Criterion
Comparison of Von Mises and Tresca yield criteria
6.2 Plastic Deformation
Slip and Twinning
Slip Systems
| Crystal Structure | Slip Plane | Slip Direction | # Slip Systems |
|---|---|---|---|
| FCC | {111} | <110> | 12 |
| BCC | {110}, {112}, {123} | <111> | 48 |
| HCP | (0001) | <11-20> | 3 |
Schmid's Law
Where φ is angle between stress axis and slip plane normal, λ is angle between stress axis and slip direction
Twinning
Twinning shear (γ) for common metals:
6.3 Dislocation Theory
Dislocation Types
Edge Dislocation
Edge dislocation with extra half-plane
Screw Dislocation
Screw dislocation with spiral ramp
Mixed Dislocation
Dislocation Dynamics
Stress Fields
Edge dislocation:
Screw dislocation:
Dislocation Energy
Where K = 1 for screw, K = 1-ν for edge dislocations
Frank-Read Source
Where L is segment length between pinning points
6.4 Strengthening Mechanisms
Work/Strain Hardening
Where n is strain hardening exponent (0.1-0.5 for metals)
Grain Boundary Strengthening (Hall-Petch)
Solid Solution Strengthening
Where c is solute concentration, ε is size misfit parameter
Precipitation Strengthening
6.5 Fracture Behavior
Griffith Theory
Where γs is surface energy, a is crack length
Modified for Plasticity
Where γp is plastic work per unit area
Linear Elastic Fracture Mechanics
Stress Intensity Factor
Where Y is geometry factor (~1 for center crack)
Fracture Toughness
Where Gc is critical strain energy release rate
Ductile-to-Brittle Transition
Where β is material constant, K̇ is loading rate
6.6 Fatigue
S-N Curve
Where σ'f is fatigue strength coefficient, b is exponent
Crack Growth (Paris Law)
Where C and m are material constants
Endurance Limit
6.7 High Temperature Deformation
Creep Stages
Norton's Law
Where n is stress exponent, Q is activation energy
Larson-Miller Parameter
Where C ≈ 20 for many metals
TestUrSelf's Course Features
Mechanical Metallurgy Mastery Course
Course Highlights
- 600+ practice problems with detailed solutions
- Interactive dislocation dynamics simulations
- 12 full-length mock tests with performance analysis
- Microstructure interpretation workshops
- Fracture surface analysis exercises
Special Modules
| Module | Topics | Problems |
|---|---|---|
| 1 | Stress-Strain Analysis | 120 |
| 2 | Dislocation Theory | 150 |
| 3 | Fracture Mechanics | 130 |
| 4 | Fatigue & Creep | 100 |
| 5 | Numerical Problem Solving | 100 |