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Title:

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

Document type:
Zeitschriftenaufsatz
Author(s):
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...     »
Keywords:
Experimental aerodynamics; Flexible wing surface; Force and moment measurements; Morphing wing; Particle image velocimetry
Dewey Decimal Classification:
620 Ingenieurwissenschaften
Journal title:
Chinese Journal of Aeronautics
Year:
2020
Covered by:
Scopus
Language:
en
Fulltext / DOI:
doi:10.1016/j.cja.2020.03.037
Publisher:
Elsevier BV
E-ISSN:
1000-9361
Submitted:
23.12.2019
Accepted:
16.02.2020
Date of publication:
01.06.2020
TUM Institution:
Lehrstuhl für Aerodynamik und Strömungsmechanik
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