93847 - Fatigue And Damage Tolerance

Academic Year 2020/2021

Learning outcomes

The student becomes familiar with the advanced methods for the evaluation of stress and strain field in aerospace structures; he/she learns and applies the main methods for the conceptual and preliminary design of aircraft. He/she also acquires in-depth knowledge of the Damage-Tolerance methodology used in the design of aerospace structures.

Course contents

  • Introduction to Fatigue (fatigue as a phenomenon; stress concentrations; residual stresses; fatigue properties of metallic and composite materials; fatigue strength of notched specimens, residual strength).
  • Fatigue damage mechanisms (initiation, crack growth, delamination growth, transverse matrix cracking, fibre failure).
  • Analysis methods (stress concentration factors, stress intensity factors; energy balance approaches, strain energy release rates).
  • Fatigue loading (Load Spectra, Fatigue under Constant- & Variable-Amplitude Loading).
  • Special Fatigue Conditions (surface treatments; fretting corrosion; corrosion fatigue; high-temperature and low-temperature fatigue, moisture ingress).
  • Fatigue and Damage Tolerance of Aircraft Structures: Regulations, tests, scatter, application of fatigue and damage tolerance methods.

Readings/Bibliography

J. Schijve, Fatigue of Structures and Materials, 2nd edition, 2009, Springer Science+Business Media, B.V., ISBN-13: 978-1-4020-6807-2 e-ISBN-13: 978-1-4020-6808-9

Teaching methods

Self-study using the Online Course Material on TUDelft's Brightspace together with weekly plenary instruction sessions and discussions with course instructors.

Assessment methods

Written exam & ungraded assignments

Office hours

See the website of Reyndert Christiaan Alderliesten

See the website of John Alan Pascoe