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


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1 Bhubaneswar Engineering College, Bhubaneswar, Odisha, India
     

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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.

Keywords

AAW, Aeroelasticiy, Conventional Approach, Wind Tunnel Model.
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  • M. H. Love, P. M. Flick, P. S. Zink, and D. N. Mavris, “Impact of active aeroelastic wing echnology on wing geometry using response surface methodology,” NASA Langley International Forum on Aeroelasticity and Structural Dynamics, Williamsburg, VA, pp. 22-25, June 1999.

  • P. S. Zink, M. H. Love, and P. M. Flick, “The impact of active aeroelastic wing technology on conceptual aircraft design,” RTO AVT Specialists’ Meeting on Structural Aspects of Flexible Aircraft Control Canada, pp. 18-20, October 1999.

  • J. Heeg, C. V. Spain, J. R. Florance, C. D. Wieseman, T. G. Ivanco, J. A. DeMoss, W. A. Silva, A. Panetta, P. Lively, and V. Tumwa, “Experimental results from the active aeroelastic wing wind tunnel test program wing wind tunnel test program,” Collection of Technical Papers- Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 8, pp. 5384-5399.

  • F. Eastep, “Development of preliminary design models for active aeroelastic wing application,”.

  • S. Heinze, “Aeroelastic concepts for flexible wing structure,” Universities service US AB Stockholm.


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

Abstract Views: 369  |  PDF Views: 0

Authors

Chinmayee Panigrahi
Bhubaneswar Engineering College, Bhubaneswar, Odisha, India
S. K. Samal
Bhubaneswar Engineering College, Bhubaneswar, Odisha, India

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 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.

Keywords


AAW, Aeroelasticiy, Conventional Approach, Wind Tunnel Model.

References