Tell a friend
Print
Silva Freitas Neto, Arnold (2022) Rigid Body and Structural Dynamics Measurement System for Flexible Aircraft. Bachelor's, Technische Universität Berlin.
Full text not available from this repository.
Abstract
Ziel der Bachelorarbeit ist es, ein elektrisches System zur geleichzeigen Messung von flugmechanischen Freiheitsgraden und dynamischen strukturellen Deformationen zu entwerfen. Das System soll am TU FLEX eingesetzt werden, einem unbemannten fliegenden Demonstrator der TU Berlin, der mit Flügeln unterschiedlicher Flexibilität eingesetzt werden kann.
| Item URL in elib: | https://elib.dlr.de/187519/ | ||||||
|---|---|---|---|---|---|---|---|
| Document Type: | Thesis (Bachelor's) | ||||||
| Title: | Rigid Body and Structural Dynamics Measurement System for Flexible Aircraft | ||||||
| Authors: |
| ||||||
| Date: | 18 April 2022 | ||||||
| Refereed publication: | No | ||||||
| Open Access: | No | ||||||
| Gold Open Access: | No | ||||||
| In SCOPUS: | No | ||||||
| In ISI Web of Science: | No | ||||||
| Number of Pages: | 65 | ||||||
| Status: | Accepted | ||||||
| Keywords: | UAV, Strukturdynamik, fliegender Demonstrator, Datenerfassung im Flugversuch | ||||||
| Institution: | Technische Universität Berlin | ||||||
| Department: | Institut für Luft- und Raumfahrt, Fachgebiet Flugmechanik, Flugregelung und Aeroelastizität | ||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||
| HGF - Program: | Aeronautics | ||||||
| HGF - Program Themes: | Efficient Vehicle | ||||||
| DLR - Research area: | Aeronautics | ||||||
| DLR - Program: | L EV - Efficient Vehicle | ||||||
| DLR - Research theme (Project): | L - Virtual Aircraft and Validation | ||||||
| Location: | Göttingen | ||||||
| Institutes and Institutions: | Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design | ||||||
| Deposited By: | Krüger, Prof. Dr.-Ing. Wolf R. | ||||||
| Deposited On: | 18 Jul 2022 13:42 | ||||||
| Last Modified: | 18 Jul 2022 13:42 |
Repository Staff Only: item control page
