AE51016: Fracture Mechanics

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AE51016
Course name Fracture Mechanics
Offered by Aerospace Engineering
Credits 3
L-T-P 3-0-0
Previous Year Grade Distribution
1







EX A B C D P F
Semester Spring


Syllabus[edit | edit source]

Syllabus mentioned in ERP[edit | edit source]

Prerequisites: AE21004 3 - 0 - 0: 3 CreditsMechanisms of fracture and crack growth, elastic crack-tip 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]