AERO

CAE343: Fatigue and Fracture Mechanics syllabus for Aero 2021 regulation (Professional Elective-III)

Fatigue and Fracture Mechanics detailed syllabus for Aeronautical Engineering (Aero) for 2021 regulation curriculum has been taken from the Anna Universities official website and presented for the Aero students. For course code, course name, number of credits for a course and other scheme related information, do visit full semester subjects post given below.

For Aeronautical Engineering 5th Sem scheme and its subjects, do visit Aero 5th Sem 2021 regulation scheme. For Professional Elective-III scheme and its subjects refer to Aero Professional Elective-III syllabus scheme. The detailed syllabus of fatigue and fracture mechanics is as follows.

Course Objectives:

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Unit I

FATIGUE OF STRUCTURES
S.N. curves – Endurance limits – Effect of mean stress, Goodman, Gerber and Soderberg relations and diagrams – Notches and stress concentrations – Neuber’s stress concentration factors – Plastic stress concentration factors – Notched S.N. curves – Fatigue of composite materials.

Unit II

STATISTICAL ASPECTS OF FATIGUE BEHAVIOUR
Low cycle and high cycle fatigue – Coffin – Manson’s relation – Transition life – cyclic strain hardening and softening – Analysis of load histories – Cycle counting techniques -Cumulative damage – Miner’s theory – Other theories.

Unit III

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Unit IV

FRACTURE MECHANICS
Strength of cracked bodies – Potential energy and surface energy – Griffith’s theory – Irwin – Orwin extension of Griffith’s theory to ductile materials – stress analysis of “cracked bodies – Effect of thickness on fracture toughness” – stress intensity factors for typical ‘geometries.

Unit V

FATIGUE DESIGN AND TESTING
Safe life and Fail-safe design philosophies – Importance of Fracture Mechanics in aerospace structures – Application to composite materials and structures.

Course Outcomes:

Students will be able to

  1. Apply the mathematical knowledge to define fatigue behaviours of the materials
  2. Identify the causes for the fatigue failure of the materials.
  3. Ability to analyse the fracture due to fatigue
  4. Select the testing method for the fatigue failure prediction of the materials.
  5. Solve the causes of the crack initiation & its growth.
  6. Select the materials with ability to with damage tolerant structures

Text Books:

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Reference Books:

  1. Kare Hellan ,’Introduction to Fracture Mechanics’, McGraw Hill, Singapore,1985
  2. Knott, J.F., “Fundamentals of Fracture Mechanics,” – Buterworth & Co., Ltd., London, 1983.
  3. Sih C.G., “Mechanics of fracture.” Vol – I, Sijthoff and w Noordhoff International Publishing Co., Netherlands, 1989.

For detailed syllabus of all the other subjects of Aeronautical Engineering 5th Sem, visit Aero 5th Sem subject syllabuses for 2021 regulation.

For all Aeronautical Engineering results, visit Anna University Aero all semester results direct link.

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