Academic year 2021/2022 |
Supervisor: | doc. Ing. Jaroslav Juračka, Ph.D. | |||
Supervising institute: | LÚ | |||
Teaching language: | Czech or English | |||
Aims of the course unit: | ||||
The goal is to familiarize students with specifics of composite materials, their application to structure design, possible technology and detail of strength analysis techniques. | ||||
Learning outcomes and competences: | ||||
Higher degree of composite structures knowledge | ||||
Prerequisites: | ||||
Graduation of Aeronautic composite structures subject. | ||||
Course contents: | ||||
Doctoral students will be acquainted with detail problems of composite structures, composite materials application to structure design, possible technology and detail techniques of strength analysis. Topics of micromechanics, and macromechanics theories, joints, 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. | ||||
Assesment methods and criteria linked to learning outcomes: | ||||
Creation and followed defence of defined topic. | ||||
Controlled participation in lessons: | ||||
Individual form of study, self studying and consultation. | ||||
Type of course unit: | ||||
Lecture | 10 × 2 hrs. | optionally | ||
Course curriculum: | ||||
Lecture | 1. Introduction 2. Structure capability. Failure criteria. Subsequent fails of composites 3. Fracture toughness 4. Virtual crack closing technique. 5. Fatigue. 6. Mechanical characteristics, testing. 7. Joints of composite structures. 8. Structure heath monitoring, NDT, repairs. 9. Quality, quality control. 10. Airworthiness requirements. |
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Literature - fundamental: | ||||
1. Reddy, J.N., mechanics of laminated composite plates and shells, Theory and Analysis | ||||
2. Baker, A., Dutton, S., Kelly, D., Composite Materials for Aircraft Structures, AIAA Edication series, ISBN 1-56347-540-5, Reston, 1999 | ||||
3. Raju, I.S.,O`Brien, T.K., Fracture mechanics concepts, stress fields, strain energy release rate, delamination initiation and growth criteria, NASA-Langley Research Centre, USA, 2008 |
The study programmes with the given course: | |||||||||
Programme | Study form | Branch | Spec. | Final classification | Course-unit credits | Obligation | Level | Year | Semester |
D-KPI-P | full-time study | --- no specialisation | -- | DrEx | 0 | Recommended course | 3 | 1 | W |
D-KPI-K | combined study | --- no specialisation | -- | DrEx | 0 | Recommended course | 3 | 1 | W |
Faculty of Mechanical Engineering
Brno University of Technology
Technická 2896/2
616 69 Brno
Czech Republic
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