27th Congress of International Council of the Aeronautical Sciences, 19 - 24 September 2010, Nice, France 
Paper      ICAS 2010-2.10.4            
EXPERIMENTAL INVESTIGATIONS OF AN ELASTO-FLEXIBLE MORPHING WING CONCEPT
                  B. Beguin, C. Breitsamter, N. Adams       
          TU Munich, Germany
Keywords:  morphing wing, membrane wing, flow control, aerodynamic efficiency    
 
Morphing technology is of great interest because it is likely to improve performances and extend flight envelope of aircrafts. In this context, an elastoflexible morphing wing concept, taking advantage of sailwing structure and allowing large changes of wing planform, is experimentally and numerically investigated.      

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