Aircraft Composite Structures (FSI-OKL)

Academic year 2018/2019
Supervisor: doc. Ing. Jaroslav Juračka, Ph.D.  
Supervising institute: LÚ all courses guaranted by this institute
Teaching language: Czech
Aims of the course unit:
The goal is to familiarize students with fundaments of composite materials, their application to structure design, possible technology and basic strength calculation.
Learning outcomes and competences:
Student will gain basic knowledge about composite materials, its application to structure design, technology and strength calculation.
Prerequisites:
Basic knowledge of strength and elastic theory.
Course contents:
Students will be acquainted with fundaments of composite materials, their application to structure design, possible technology and basic strength calculation. Topics of micromechanics, macromechanics, joints, stability, quality assurance, application at structure and testing will be presented.
Teaching methods and criteria:
The course is taught through lectures explaining the basic principles and theory of the discipline. Exercises are focused on practical topics presented in lectures. Teaching is suplemented by practical laboratory work.
Assesment methods and criteria linked to learning outcomes:
Course-unit credit: 90% participation in exercises, completion of all calculated task from exercises. Exam: written test - theoretical background, task calculation
Controlled participation in lessons:
Participation in lectures and exercises. Missed exercises will be compensated by self-study of tasks.
Type of course unit:
    Lecture  13 × 2 hrs. optionally                  
    Exercise  12 × 1 hrs. compulsory                  
    Labs and studios  1 × 1 hrs. compulsory                  
Course curriculum:
    Lecture 1. Introduction. Fibres, matrix.
2. Basic characteristics of composites. Micromechanics.
3. Manufacture and component form.
4. Macromechanic.
5. Capability. Failure criteria.
6. Stability. Sandwich structure.
7. Mechanical property, testing.
8. Properties of composite system.
9. Joining of composite structure.
10. Repair technology.
11. Quality assurance.
12. Airworthiness considerations.
13. Structure Application. Tests.
    Exercise 1. Material selection for application.
2. Mixture rule. Influence of orientation.
3. Lamina stiffness matrix.
4. Laminate stiffness matrix. Stiffness characteristics.
5. Failure criteria.
6. Failure envelope.
7. Bonding joints.
8. Mechanical joints.
9. Stability.
10. Sandwich structure.
11. Repair design.
12. Test design.
    Labs and studios 1. Testing of mechanical properties.
Literature - fundamental:
1. Alan Baker,Stuart Dutton,Donald Kelly, Composite Materials for Aircraft Structure, AIAA
2. Mahmood Husein Datoo, Mechanics of Fibrous Composites, ISBN 1-85166-600-1, Elsevier Science Publishers, 1991
Literature - recommended:
3. Middelton, D. H., Compozite materials in aircraft structures, 1st ed., London, Longman Grup, 1990, ISBN: 0-582-01712-2
The study programmes with the given course:
Programme Study form Branch Spec. Final classification   Course-unit credits     Obligation     Level     Year     Semester  
M2I-P full-time study M-STL Aircraft Design -- Cr,Ex 4 Compulsory 2 1 S