Diploma in Damage Tolerance and Fatigue Life of Aerostructures
About us Diploma in Damage Tolerance and Fatigue Life of Aerostructures
The Diploma in Damage Tolerance and Fatigue Life of Aerostructures focuses on the study of aircraft structural integrity, addressing damage and fatigue analysis in key components. It centers on the design and evaluation of structures capable of tolerating damage and resisting load cycles, using finite element analysis (FEA) and destructive (DT) and non-destructive testing (NDT) tools. Methods for predicting the service life of structures and evaluating crack propagation are studied, linked to aeronautical certification. The program provides practical skills in the application of international norms and standards, such as those related to aviation safety, including stress analysis simulation. This prepares professionals for roles such as structural integrity engineers, fatigue analysts, and airframe design and certification specialists, increasing their value in the aerospace industry.
Target keywords (natural in the text): damage tolerance, fatigue life, aeroframes, FEA analysis, NDT testing, aerospace certification, structural integrity, crack propagation.
Diploma in Damage Tolerance and Fatigue Life of Aerostructures
- Format:
- Duration:
- Hours: 900 H
- Language:
- Credits:
- Registration date: 08-09-2026
- Strat date: 19-10-2026
- Available places: 11
899 $
Competencies and results
What you will learn
Who this program is for:
Diploma in Damage Tolerance and Fatigue Life of Aerostructures
Module 9 — Aerostructures: Aeronautical Principles and Regulations
9.9 Introduction to aerostructures and their importance in naval aviation.
9.9 Fundamental principles of mechanics of materials applied to aircraft.
9.3 Loads and stresses in aerostructures: types and analysis.
9.4 Aeronautical materials: properties, selection, and applications.
9.5 Design and manufacturing of structural components.
9.6 Aeronautical regulations: FAR/JAR/EASA and their application.
9.7 Certification requirements for aircraft and aerostructures.
9.8 Quality control and non-destructive testing (NDT).
9.9 Introduction to fatigue life and damage tolerance.
9.90 Case studies: examples of structural failures and lessons learned.
Capstone-type projects
Admissions, fees and scholarships
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