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
Supervisor
Department
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.