FSI-OS1Acad. year: 2018/2019
Design and stress analysis of aircraft wing according to individual assignments. A practical application of International Airworthiness Requirements, aerodynamic design and load of structures.
Learning outcomes of the course unit
Application of practical knowledge from lectures on aircraft wing design.
Basic knowledge of aircraft design and aircraft structure strength. Orientation in aviation requirements.
Recommended optional programme components
Recommended or required reading
Roskam, J.: Airplane design – Part V: Component weight estimation, Roskam aviation and engineering corporation, Ottawa, 1985. (EN)
ČALKOVSKÝ A., Konstrukce a pevnost letadel, VAAZ, 1984
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.
Language of instruction
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.
Type of course unit
seminars in computer labs
39 hours, compulsory
Teacher / Lecturer
Students make project individually with consultations. Students can use literature, SW and HW at the Institute.