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Titel:

Gust response of an elasto-flexible morphing wing using fluid–structure interaction simulations

Dokumenttyp:
Zeitschriftenaufsatz
Autor(en):
PFLÜGER, Jonathan; BREITSAMTER, Christian
Abstract:
Small and micro unmanned aircraft are the focus of scientific interest due to their wide range of applications. They often operate in a highly unstable flight environment where the application of new morphing wing technologies offers the opportunity to improve flight characteristics. The investigated concept comprises port and starboard adjustable wings, and an adaptive elasto-flexible membrane serves as the lifting surface. The focus is on the benefits of the deforming membrane during the impac...     »
Stichworte:
Computational fluid dynamics; Flexible wing surface; Fluid-structure interaction; Gust response; Membrane wing; Morphing wing; Unsteady inflow condition
Dewey Dezimalklassifikation:
620 Ingenieurwissenschaften
Zeitschriftentitel:
Chinese Journal of Aeronautics
Jahr:
2024
Band / Volume:
37
Heft / Issue:
2
Seitenangaben Beitrag:
45-57
Nachgewiesen in:
Scopus
Sprache:
en
Volltext / DOI:
doi:10.1016/j.cja.2023.12.017
Verlag / Institution:
Elsevier BV
E-ISSN:
1000-9361
Hinweise:
Funding text 1 The project is funded by the Deutsche Forschungsgemeinschaft (DFG, German Research Foundation) (No. BR 1511/12-1). The authors want to thank ANSYS for providing the fluid-structure interaction simulation software. Furthermore, the authors gratefully acknowledge the Leibniz Rechenzentrum for providing resources at the Linux Cluster and extensive technical support. Funding text 2 The project is funded by the Deutsche Forschungsgemeinschaft (DFG, German Research Foundation) (No. B...     »
Eingereicht (bei Zeitschrift):
29.06.2023
Angenommen (von Zeitschrift):
19.10.2023
Publikationsdatum:
01.02.2024
TUM Einrichtung:
Lehrstuhl für Aerodynamik und Strömungsmechanik
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