Diploma Project

Course guarantor:

Lecturer:

Tutor:

Supervisor:

Department of Aerospace Engineering

Synopsis:

Dissertation is assigned according to practical needs of the industry or according to research and development intentions of the University.

Design of an aircraft construction or its part, its aerodynamic analysis, determination of load, stress control, proposal of production technology and preparation and execution of test under the leadership of the head of the dissertation and the consultants.

Requirements:

Work on the assigned project requires complex knowledge from the field of aerospace technology. It is necessary to pass the following courses:

Mathematics IV.

Momentum, Mass and Heat Transfer

Aircraft Design

Aircraft Propulsion

Airplane Structures and Design I.

Airplane Structures and Design II.

Aircraft Systems

Fundamentals of Aerodynamics

Low Speed Aerodynamics

High Speed Aerodynamics

Mechanics of Flight I.

Mechanics of Flight I.

Strength of Materials II.

Strength of aircraft and engines

Fatigue Life of aircraft and engines

Reliabibility of Aerospace Engineering

Materials in Aircraft Engineering

Project - Aerospace Engineering

Project I. - Aircraft Design

Project II. - Aircraft Design

Syllabus of lectures:

Syllabus of tutorials:

Study Objective:

The goal of the dissertation is to prove creative ingeneering skills of the master student and his/her ability to individually solve the assigned task under the leadership of the dissertation head and the consultants. The dissertation is done in the fields of aircraft construction, its aerodynamics and stress analysis, production technology, or tests.

Study materials:

Assigned by the head of dissertation 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: