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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Published in: | Journal of intelligent material systems and structures Vol. 19; no. 9; pp. 1101 - 1112 |
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Main Authors: | , , , , |
Format: | Journal Article |
Language: | English |
Published: |
London, England
SAGE Publications
01-09-2008
Technomic |
Subjects: | |
Online Access: | Get full text |
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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. |
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Bibliography: | ObjectType-Article-2 SourceType-Scholarly Journals-1 ObjectType-Feature-1 content type line 23 |
ISSN: | 1045-389X 1530-8138 |
DOI: | 10.1177/1045389X08096734 |