ANWESH: International Journal of Management & Information Technology

1. Chinmayee Panigrahi – Bhubaneswar Engineering College, Bhubaneswar, Odisha, India

2. S. K. Samal – Bhubaneswar Engineering College, Bhubaneswar, Odisha, India

Received
20-Jan-2017
Accepted
-
Published
20-Jan-2017
Abstract
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 behavior 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 inter-gradations of flight control, aerodynamic control, and structural performance.
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