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Titel:

Flow Field and Deformation Measurements of a Membrane Wing for Unsteady Inflow Conditions

Dokumenttyp:
Konferenzbeitrag
Autor(en):
Pflüger, Jonathan; Breitsamter, Christian
Abstract:
Unmanned and micro aerial vehicles operate in a highly unsteady flight environment. The application of morphing wing technologies for these aircraft offer the possibility to improve flight characteristics. The investigated concept consists of port and starboard adjustable wings, which are covered by an elasto-flexible membrane. For wind tunnel investigations at low Reynolds numbers the aspect ratio and the sweep of the wings can be changed. Especially interesting for the present study is the def...     »
Dewey-Dezimalklassifikation:
620 Ingenieurwissenschaften
Kongress- / Buchtitel:
AIAA AVIATION 2022 Forum
Verlag / Institution:
American Institute of Aeronautics and Astronautics
Publikationsdatum:
20.06.2022
Jahr:
2022
Nachgewiesen in:
Scopus
Sprache:
en
Volltext / DOI:
doi:10.2514/6.2022-3895
WWW:
https://arc.aiaa.org/doi/abs/10.2514/6.2022-3895
Hinweise:
Funding text The project is funded by the Deutsche Forschungsgemeinschaft (DFG, German Research Foundation) grant number BR 1511/12-1.
TUM Einrichtung:
Lehrstuhl für Aerodynamik und Strömungsmechanik
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