Project IV.

The course is not on the list Without time-table
Code Completion Credits Range Language
2222100 KZ 5 0P+5C Czech
Garant předmětu:
Department of Aerospace Engineering

The assignment of Project IV mostly comes from practical needs of the industry or the research and development intentions of the University.

Modification of the 3D model of the construction solution created in Project III and its repeated stress analysis for the defined load. Working out of the final version of the 3D model and drawing of necessary documentation required by the assignment. Working out a technical report and defending the project in presentation.

In case a different character is assigned (flow, stress analysis, technology experiment), the tutor will formulate the subject to enable continuation in Project III. The formal condidtion to fulfill the project requirements are the same as in the assignment of a construction character.


Completion of compulsory and choice-compulsory subjects of the first, second and third semester of master's degree in Aerospace Technology, unconditionally Project II and III.

Parallel with the overlapping compulsory and choice-compulsory subjects in the forth semester of master's degree in Aerospace Technology.

Syllabus of lectures:
Syllabus of tutorials:

The basic point will be assigned according to assignment by the tutor of the course.

Study Objective:

Work out the final version of a construction solution in form of a 3D model and documentation required by assignment. Work out and defend in a presentation a final technical report containing the description of the final construction solution, definition of load, stress analysis and required documentation.

In case a different character is assigned (flow, stress analysis, technology, experiment), the tutor will assign the project goals in a way to enable continuation of Project III.

Study materials:

-E. Torenbeek: Synthesis of Subsonic Airplane Design, Kluwer Academis Publishers, Delft 1982, ISBN 90-247-2724-3

-Roskam J.: Airplane Desing, Roskam Aviation and Engineering Corporation, 1985

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

-Other literature - Assigned by the head of dissertation according to assigned theme

Further information:
No time-table has been prepared for this course
The course is a part of the following study plans:
Data valid to 2024-06-16
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