Course detail

Semester Project

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.

Prerequisites

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

Co-requisites

Not applicable.

Recommended optional programme components

Not applicable.

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

Czech

Work placements

Not applicable.

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.

Classification of course in study plans

  • Programme M2I-P Master's

    branch M-STL , 1. year of study, summer semester, 4 credits, compulsory

Type of course unit

 

seminars in computer labs

39 hours, compulsory

Teacher / Lecturer

Syllabus

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