Branch Project II.

Course guarantor:

Lecturer:

Tutor:

Supervisor:

Department of Aerospace Engineering

Synopsis:

The Branch Project assignment is largely based on the practical needs of the industry or the research and development objectives of the university.

The content is a structural design of a selected part of the airplane structure including the creation of a 3D model of the designed structure, determination of the loading and the stress analysis, proposition and execution of experiment on designed part of structure (if required).

The conclusion is a technical report describing the proposed solution

Requirements:

Completion of subjects Branch Project I and Aeronautics and Astronautics.

Syllabus of lectures:

Syllabus of tutorials:

Individual according to the assigned theme under the supervision of the bachelor thesis supervisor.

Study Objective:

The aim of the course is to master the design of a structural solution in the field of aircraft technology, including 3D modeling, loading determination and basic stress analysis in time.

Study materials:

- D. P. Raymer: Aircraft Design: A Conceptual Approach, AIAA Education Series, Washington 1989, ISBN 0-930403-51-7

- Other literature - Assigned by the supervisor of bachelor thesis according to assigned theme

Note:

Further information:

No time-table has been prepared for this course

The course is a part of the following study plans: