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This document provides a summary of a licentiate thesis on strength analysis and modeling of hybrid composite-aluminum aircraft structures. The thesis covers: 1. Material characterization of composites and aluminum, including static strength, stiffness, and fatigue damage development. 2. Certification requirements for aircraft structures, including analysis and testing. 3. Constitutive modeling approaches for elastic behavior, failure criteria, and damage progression. 4. Finite element modeling techni

Author

sheberua

Language

EN