Semester Project (FSI-OS1)

Academic year 2019/2020
Supervisor: doc. Ing. Ivo Jebáček, Ph.D.  
Supervising institute: LÚ all courses guaranted by this institute
Teaching language: Czech
Aims of the course unit:
The goal is to design a required aircraft part and to make necessary aerodynamic and strength analyses.
Learning outcomes and competences:
Application of practical knowledge from lectures on aircraft wing design.
Prerequisites:
Basic knowledge of aircraft design and aircraft structure strength. Orientation in aviation requirements.
Course contents:
Design and stress analysis of aircraft wing according to individual assignments. A practical application of International Airworthiness Requirements, aerodynamic design and load of structures.
Teaching methods and criteria:
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.
Controlled participation in lessons:
Participation in the first seminar.
Type of course unit:
    Computer-assisted exercise  13 × 3 hrs. compulsory                  
Course curriculum:
    Computer-assisted exercise Students make project individually with consultations. Students can use literature, SW and HW at the Institute.
Literature - fundamental:
1. ČALKOVSKÝ A., Konstrukce a pevnost letadel, VAAZ, 1984
Literature - recommended:
1. Roskam, J.: Airplane design – Part V: Component weight estimation, Roskam aviation and engineering corporation, Ottawa, 1985.
The study programmes with the given course:
Programme Study form Branch Spec. Final classification   Course-unit credits     Obligation     Level     Year     Semester  
M2I-P full-time study M-STL Aircraft Design -- GCr 4 Compulsory 2 1 S