Mastering advanced structural analysis methods applied to flying vehicles composite sturctures.

In the end of completed course students should be able to: 1. master theoretical knowledge in stress strain analysis of composite structures used in aerospace. 2. apply presented methods in solving real problems related to composite aerospace structures and composite structures in general.

Elastic behaviour of multidirectional laminates symmetric laminates, balanced laminates Quasi-isotropic laminates Temperature effectes on laminate stress strain, analysis methods Laminate Failure analysis Types of laminate failure Strength analaysis FPF theory experimantal methods in laminate characterization

Stress strain analysis of complex composite structures using finite elements approach.

Structural analayis, composite structures

laboratory for Theory of elasticity and aeroelasticity

Total assigned hours: 65

New material: 30
Elaboration and examples (recapitulation): 20

Auditory exercises: 0
Laboratory exercises: 0
Calculation tasks: 0
Seminar paper: 0
Project: 0
Consultations: 0
Discussion/workshop: 0
Research study work: 0

Review and grading of calculation tasks: 5
Review and grading of lab reports: 0
Review and grading of seminar papers: 10
Review and grading of the project: 0
Test: 0
Test: 0
Final exam: 0

Activity during lectures: 0
Test/test: 0
Laboratory practice: 0
Calculation tasks: 0
Seminar paper: 0
Project: 50
Final exam: 50
Requirement for taking the exam (required number of points): 0

Structural Composites: Advanced Composites in Aviation by Ronald Sterkenburg and Peng Hao Wang (2013); Advanced Mechanics of Composite Materials and Structural Elements, Third Edition by V.V. Vasiliev 2007; Advanced Mechanics of Composite Materials and Structural Elements, Third Edition by V.V. Vasiliev 2007