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Document type:
Zeitschriftenaufsatz 
Author(s):
PFLÜGER, Jonathan; BREITSAMTER, Christian 
Title:
Experimental investigations of a full model with adaptive elasto-flexible membrane wings 
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 
Publisher:
Elsevier BV 
E-ISSN:
1000-9361 
Accepted:
16.02.2020 
Date of publication:
01.06.2020 
TUM Institution:
Lehrstuhl für Aerodynamik und Strömungsmechanik