Design, Analysis and Experimental Evaluation of Active Aeroelastic Wing (AAW) Technology

This paper summarizes the design, analysis and experimental evaluation of Active Aeroelastic Wing (AAW) technology and is need over conventional design process. The results provide control derivatives of control surface of an aircraft by using AAW design. Also the result indicates some different behaviour which was not expected while doing the conceptual design. It is multidisciplinary study in engineering technology. This is a new technology in the area of structural design approach. This is a intergradations of flight control, aerodynamic control, and structural performance.