Course detail

Aerostructures Capability

FSI-OPK-A Acad. year: 2024/2025 Summer semester

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

English

Number of ECTS credits

5

Supervisor

doc. Ing. Jaroslav Juračka, Ph.D.

Department

Institute of Aerospace Engineering

Entry knowledge

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

Rules for evaluation and completion of the course

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.
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

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

The study programmes with the given course

Programme N-AST-A: Aerospace Technology, Master's, compulsory

Type of course unit

 

Lecture

52 hours, compulsory

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 hours, compulsory

Syllabus

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

Exercise

22 hours, compulsory

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.