Course detail

Semester Project

FSI-OS1-A Acad. year: 2019/2020 Summer semester

Design and stress analysis of aircraft wing according to individual assignments. A practical application of International Airworthiness Requirements, aerodynamic design and load of structures.

Language of instruction

English

Number of ECTS credits

4

Learning outcomes of the course unit

Application of practical knowledge from lectures on aircraft wing design.

Prerequisites

Basic knowledge of aircraft design and aircraft structure strength. Orientation in aviation requirements.

Planned learning activities and teaching methods

The course is taught through exercises which are focused on practical topics presented in lectures.

Assesment methods and criteria linked to learning outcomes

Course-unit credit requirements: submitting the report in a prescribed form and in time , positive evaluation of student’s work by a course guarantor. The evaluation of work is done individually and in accordance with FME BUT rules.

Aims

The goal is to design a required aircraft part and to make necessary aerodynamic and strength analyses.

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

Participation in the first seminar.

The study programmes with the given course

Programme M2E-A: Industrial Engineering, Master's
branch M-IND: Industrial Engineering, compulsory

Programme M2I-A: Mechanical Engineering, Master's
branch M-STL: Aircraft Design, compulsory

Type of course unit

 

Computer-assisted exercise

39 hours, compulsory

Teacher / Lecturer

Syllabus

Students make project individually with consultations. Students can use literature, SW and HW at the Institute.