AE60036: Fracture Mechanics

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Offered by Aerospace Engineering
Credits 3
L-T-P 3-0-0
Previous Year Grade Distribution
Semester {{{semester}}}

Syllabus[edit | edit source]

Syllabus mentioned in ERP[edit | edit source]

Prerequisites: AE60005Mechanisms of fracture and crack growth, elastic cracktip stress field, crack-tip plastic zones, stress intensity factor, Energy principle and criteria for crack growth, Plane strain and plane stress fracture toughness, crack-opening displacement criterion, fatigue crack propagation under constant and variable amplitude loading, crack closure, effective stress intensity range, Concept of safe-life, fail-safe and damage tolerance in aircraft design, Linear damage accumulation theory, Aircraft safe fatigue life.

Concepts taught in class[edit | edit source]

Student Opinion[edit | edit source]

How to Crack the Paper[edit | edit source]

Classroom resources[edit | edit source]

Additional Resources[edit | edit source]