The lecture „Aircraft Design“ engross, based on the course „Fundamentals of Aeronautical Engineering“, different current design methods and major designing tools. They will be applicable for the practical design of civil and military fixed wing aircrafts. The students acquire knowledge of systematic procedure of the aircraft design process and should be able to design assemblies with focus on the overall aircraft design as well as the overall aircraft design itself. Due to that, the required aircraft performance, current safety, economic efficiency, comfort and environmental requirements are the basics of the design process. Especially the connection between requirements and their impact on configuration level will be outlined.
|Lecturer||Prof. Dr.-Ing. Mirko Hornung|
|Schedule||2 lecture units and 1 exercise course unit per week (3 SWS)|
Assemblies and subsystems
Weight, mass and structural design
Electrical aircraft technologies
|Registration and further information on the lecture:||TUMonline|
|Registration and further information on the exercise course:||TUMonline|