Course detail

Semester Project

FSI-OS1Acad. year: 2010/2011

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

Czech

Number of ECTS credits

Mode of study

Not applicable.

Guarantor

doc. Ing. Ivo Jebáček, Ph.D.

Department

Institute of Aerospace Engineering (LÚ)

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.

Planned learning activities and teaching methods

Teaching methods depend on the type of course unit as specified in the article 7 of BUT Rules for Studies and Examinations.

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.

Course curriculum

Not applicable.

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.

Recommended optional programme components

Not applicable.

Prerequisites and corequisites

Not applicable.

Basic literature

ČALKOVSKÝ A., Konstrukce a pevnost letadel, VAAZ, 1984

Type of course unit

Computer-assisted exercise

39 hod., compulsory

Teacher / Lecturer

doc. Ing. Ivo Jebáček, Ph.D.

Syllabus

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

VUT

Faculties

University Institutes

Parts

Semester Project

Type of course unit