Mechanization of a High Aspect Ratio Wing for Aerodynamic Control

Investigations are conducted to mechanize a controlled spanwise-varying airfoil camber change for a high aspect ratio wing, resulting in optimized aerodynamic performance for a aircraft that changes weight by 50% over its mission. Mechanisms to achieve these shape changes are designed based on two s...

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Bibliographic Details
Published in:Journal of intelligent material systems and structures Vol. 19; no. 9; pp. 1101 - 1112
Main Authors: Frank, Geoffrey J., Joo, James J., Sanders, Brian, Garner, David M., Murray, Andrew P.
Format: Journal Article
Language:English
Published: London, England SAGE Publications 01-09-2008
Technomic
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Summary:Investigations are conducted to mechanize a controlled spanwise-varying airfoil camber change for a high aspect ratio wing, resulting in optimized aerodynamic performance for a aircraft that changes weight by 50% over its mission. Mechanisms to achieve these shape changes are designed based on two separate design methodologies: a rigid body kinematics approach and a compliant mechanism approach. A framework for optimizing mechanisms based on each approach is presented. Differences between the approaches are illustrated through the design of a mechanism for a specific set of airfoil shapes. Mechanisms are evaluated based on the error in the shapes and on the energy efficiency of the systems.
Bibliography:ObjectType-Article-2
SourceType-Scholarly Journals-1
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ISSN:1045-389X
1530-8138
DOI:10.1177/1045389X08096734