Course detail

Aerostructures Capability

FSI-OPKAcad. year: 2022/2023

Comprehensive overview of of stress calculation , deformation and load-bearing capacity of thin-walled structures. Methods of weight reduction and efficient use of material. Stability of rods and walls. Calculations of load-bearing capacity of spar and semi-monocoque thin-walled structures. Calculations of aircraft parts. Sandwich construction.

Language of instruction

Czech

Number of ECTS credits

5

Mode of study

Not applicable.

Guarantor

doc. Ing. Jaroslav Juračka, Ph.D.

Department

Institute of Aerospace Engineering (LÚ)

Learning outcomes of the course unit

The course enables students to realize typical calculations of aircraft thin-walled structures in non-linear areas of loading.

Prerequisites

The basic knowledge of mathematics, mechanics, structure and strength. Passing of OSZ-A Aircraft design course.

Co-requisites

Not applicable.

Planned learning activities and teaching methods

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

Conditions for the course-unit credit award: participation in lessons (80% at least), presentation of the report elaboration from laboratory exercises. The exam has written (theoretical part and practical exercises) and oral parts.

Course curriculum

Not applicable.

Work placements

Not applicable.

Aims

The goal is to familiarize students with the most important airworthiness requirements, to explain the theoretical basis of tension calculations and deformation of thin-walled aircraft structures. Students will acquire theoretical and practical knowledge of stability of rods and walls.

Specification of controlled education, way of implementation and compensation for absences

Lectures are not compulsory, attendance is registrated. Exercises are compulsory, and the attendance (80% at least) is checked and recorded. The absence (in justifiable cases) can be compensated by personal consultation with the lecturer and elaboration of individually assigned topics and exercises. Individual tasks must be finished and handed in the week course-unit credits are awarded at the latest

Recommended optional programme components

Not applicable.

Prerequisites and corequisites

Not applicable.

Basic literature

Bruhn, E.F., Analysis and Design of Flight vehicle structures, Jacobs Publishing, USA, 1973 (EN)
Čalkovský, A., Pávek, J., Daněk, V.: Konstrukce a pevnost letadel, VAAz, Brno 1984 (CS)
Niu, m. C., Airframe Structural Design, Hong KonG ConMilit Press, ISBN 962-7128-09-0, Hong kong, 1988 (EN)

Recommended reading

Not applicable.

Elearning

eLearning: currently opened course

Classification of course in study plans

  • Programme N-LKT-P Master's

    specialization STL , 1 year of study, summer semester, compulsory

  • Programme LLE Lifelong learning

    branch CZV , 1 year of study, summer semester, compulsory

Type of course unit

 

Lecture

52 hod., compulsory

Teacher / Lecturer

doc. Ing. Jaroslav Juračka, Ph.D.

Syllabus

  1. Introduction, Thin-walled structures.
  2. Limit states of materials.
  3. Stability of bars, influence of combined load. Stability of walls, influence of curvature and boundary conditions.
  4. Spar with thin web.
  5. Spar structures as box structures.
  6. Capacity of spar, semi-monocoque and monocoque structures.
  7. Method of proportional loading.
  8. Sandwich panel analysis.
  9. FEM modelling and analysis.
  10. Optimization of aircraft structures in terms of weight savings.

Laboratory exercise

4 hod., compulsory

Teacher / Lecturer

doc. Ing. Jaroslav Juračka, Ph.D.

Syllabus

1. Laboratory static tests of rods.
2. Laboratory static tests of walls.
3. Attendance on the aircraft structure test.

Exercise

22 hod., compulsory

Teacher / Lecturer

doc. Ing. Jaroslav Juračka, Ph.D.
Ing. Lukáš Dubnický, Ph.D.

Syllabus

  1. Load definition and stress analysis of landing gear.
  2. Wing load calculation.
  3. Calculation of Centre of Shear.
  4. Hinge stress analysis.
  5. Bar crimpling.
  6. Panel buckling.
  7. Spar with unstable web - application of theory.
  8. Rib analysis.
  9. Calculation of cross sections capability.
  10. Sandwich panel analysis.

Elearning

eLearning: currently opened course