Astraios PhD Opportunities1203
hasCourse

Aircraft construction  

Description

Evolution of aircrafts and helicopters design, classifications. Forces operating on airplane and helicopter. Static and dynamic loads. Overload factor, disposable overload, limitations. Load curve. Wing and rotor blade loads. Loads on ailerons, flaps and spoilers and control system. Fuselage and landing gear loads. Design trend analysis. Preliminary mass estimation. Wing, blade, fuselage, land- ing gear, mechanisation elements of control systems. Airframe and propulsion system interaction.

Delivery mode

Presential
English

Name

Aircraft construction
English

UNIVERSITY OF TWENTE

Faculty of Geo-Information Science and Earth Observation

Astraios home page

Funded by the European Union. Views and opinions expressed are however those of the author(s) only and do not necessarily reflect those of the European Union or HaDEA. Neither the European Union nor the granting authority can be held responsible for them. The statements made herein do not necessarily have the consent or agreement of the ASTRAIOS Consortium. These represent the opinion and findings of the author(s).