18   Artículos

 
en línea
Jafar S. Pilakkadan, Rafic M. Ajaj, Zawar Haider and Mohammadreza Amoozgar    
This paper studies the aeroelastic behavior of a rectangular, cantilever wing equipped with the spanwise morphing trailing edge (SMTE) concept. The SMTE consists of multiple trailing edge flaps that allow controlling the spanwise camber distribution of a... ver más
Revista: Aerospace    Formato: Electrónico

 
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
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
Muhammed S. Parancheerivilakkathil, Zawar Haider, Rafic M. Ajaj and Mohammadreza Amoozgar    
This paper presents the development of a novel polymorphing wing capable of Active Span morphing And Passive Pitching (ASAPP) for small UAVs. The span of an ASAPP wing can be actively extended by up to 25% to enhance aerodynamic efficiency, whilst its pi... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Rafic M. Ajaj, Erick I. Saavedra Flores, Mohammadreza Amoozgar and Jonathan E. Cooper    
This paper presents a parametric study on the aeroelasticity of cantilever wings equipped with Flared Hinge Folding Wingtips (FHFWTs). The finite element method is utilized to develop a computational, low-fidelity aeroelastic model. The wing structure is... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Josh Mills and Rafic Ajaj    
This paper presents an experimental investigation on using FOLDing wingtips sERving as cONtrol effectorS (FOLDERONS) for a mini Unmanned Aerial Vehicle (UAV). A representative off-the-shelf mini-UAV with a conventional configuration was selected. The mai... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Rafic Ajaj    
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Revista: Aerospace    Formato: Electrónico

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