10   Artículos

 
en línea
Zawar Haider, Rafic M. Ajaj and Lakmal Seneviratne    
This paper studies the effect of morphing rate on the aeroelasticity of a polymorphing wing capable of active span extension and passive twist/pitch. A variable domain size finite element model is developed to capture the dynamic effects due to the prese... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Hui Yang, Songcheng Jiang, Yan Wang and Hong Xiao    
A multi-dimensional morphing wing skeleton mechanism is proposed with double-sided triangular pyramid units, which can realize continuous variable span-wise bend, span-wise twist, and sweep. A lockable morphing unit is designed, and its mechanism/structu... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Zawar Haider, Rafic M. Ajaj and Lakmal Seneviratne    
This paper presents an aeroelastic analysis of a polymorphing wing capable of active span extension and passive pitch variation. The wing is split into two segments: an inboard segment responsible for span extension/retraction and an outboard segment cap... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Peter L. Bishay and Christian Aguilar    
Although the benefits of morphing wings have been proven in many studies in the last few decades, the wing skin design remains one of the challenges to advancing and implementing the morphing technology. This is due to the conflicting design requirements... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Yavuz Yaman, Ilhan Ozan Tunçöz, Yosheph Yang, Pinar Arslan, Ugur Kalkan, Harun Tiras, Ercan Gürses, Melin Sahin and Serkan Özgen    
The idea of morphing is drawing extensive attention in aerospace technologies. Several different approaches like span, camber, twist, and sweep are finding applications. In this work, the concept of a trailing edge control surface which is capable of per... ver más
Revista: Aerospace    Formato: Electrónico

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