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Titel:

Experimental investigations of a full model with adaptive elasto-flexible membrane wings

Dokumenttyp:
Zeitschriftenaufsatz
Autor(en):
PFLÜGER, Jonathan; BREITSAMTER, Christian
Abstract:
The morphing wing concept aims to constantly adapt the aerodynamics to different flight stages. The wing is able to adapt to different flight conditions by an adjustable Aspect Ratio (AR) and sweep. A high AR configuration provides high aerodynamic efficiency, while a low AR configuration, with highly swept wings offers a good maneuverability. Additionally, the flexible membrane allows the wing surface to stretch and contract in-plane as well as the airfoil to adapt to different aerodynamic load...     »
Stichworte:
Experimental aerodynamics; Flexible wing surface; Force and moment measurements; Morphing wing; Particle image velocimetry
Dewey Dezimalklassifikation:
620 Ingenieurwissenschaften
Zeitschriftentitel:
Chinese Journal of Aeronautics
Jahr:
2020
Nachgewiesen in:
Scopus
Sprache:
en
Volltext / DOI:
doi:10.1016/j.cja.2020.03.037
Verlag / Institution:
Elsevier BV
E-ISSN:
1000-9361
Eingereicht (bei Zeitschrift):
23.12.2019
Angenommen (von Zeitschrift):
16.02.2020
Publikationsdatum:
01.06.2020
TUM Einrichtung:
Lehrstuhl für Aerodynamik und Strömungsmechanik
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