6   Artículos

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en línea
Charalampos Themistokleous, Nikolaos-Grigorios Markatos, John Prospathopoulos, Vasilis Riziotis, Giorgos Sieros and George Papadakis    
Morphing offers an attractive alternative compared to conventional hinged, multi-element high lift devices. In the present work, morphed shapes of a NACA 64A010 airfoil are optimized for maximum lift characteristics. Deformed shapes of the leading and tr... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Han Bao, Bifeng Song, Wenqing Yang, Jianlin Xuan and Dong Xue    
Birds in nature have many unique devices to help them acquire excellent flight abilities under various complex flight conditions. One of the unique devices is the leading-edge alula, located at the junction of the arm wing and the hand wing of most birds... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
William Bissonnette and Götz Bramesfeld    
High-lift devices are commonly modelled using potential flow methods at the conceptual design stage. Often, these analyses require the use of prescribed wake shapes in order to avoid numerical stability issues. The wake type used, however, has an impact ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
William Bissonnette and Götz Bramesfeld    
High-lift devices are commonly modelled using potential flow methods at the conceptual design stage. Often, these analyses require the use of prescribed wake shapes in order to avoid numerical stability issues. The wake type used, however, has an impact ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Xiaotian Niu, Jie Li, Heng Zhang and Zhao Yang    
The aileron is one of the most important tools for adjusting the roll attitude of the aircraft, but the surface flow state of the aileron is likely to be affected by high-lift devices. In this paper, by using computational fluid dynamics (CFD) simulation... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Matthias Bauer, Thomas Grund, Wolfgang Nitsche and Vlad Ciobaca    
This paper discusses wind tunnel test results aimed at advancing active flow control technology to increase the aerodynamic efficiency of an aircraft during take-off. A model of the outer section of a representative civil airliner wing was equipped with ... ver más
Revista: Aerospace    Formato: Electrónico

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