Preliminary airfoil design of an innovative adaptive variable camber compliant wing
نویسندگان
چکیده
منابع مشابه
Topological Optimization of Compliant Adaptive Wing Structure
Load-path-based topology optimization is used to synthesize a compliant adaptive aircraft wing leading edge, which deforms in a prescribed way when subject to a single point internal actuation. The load-path-based optimization method requires the specification of a parent lattice. Increasing the complexity of this lattice means the number of parameters required for a complete representation of ...
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This chapter describes a new intelligent platform for learning optimal designs of morphing wings based on Variable Camber Continuous Trailing Edge Flaps (VCCTEF) in conjunction with a leading edge flap called the Variable Camber Krueger (VCK). The new platform consists of a Computational Fluid Dynamics (CFD) methodology coupled with a semi-supervised learning methodology. The CFD component of t...
متن کاملVariable-complexity optimization applied to airfoil design
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Nhan T. Nguyen a NASA Ames Research Center, Moffett Field, CA 94035 Nathan Precup b and Eli Livne c University of Washington, Seattle, WA 98195 James Urnes, Sr. d Boeing Research & Technology, St. Louis, MO 63134 Eric Dickey e Boeing Research & Technology, Huntington Beach, CA Chester Nelson f Boeing Commercial Airplanes, WA 98124 Jonathan Chiew g Stanford University, Stanford, CA 94305 David L...
متن کاملTopology Optimization of Adaptive Compliant Aircraft Wing Leading Edge
A network analysis technique is introduced which may be used for determining and parameterizing the load paths in a lattice structure to enable a load path-based topology optimization to be carried out in a way that permits the use of Genetic Algorithms. This technique provides the designer with a greater level of control over the problem complexity than alternative schemes and enables the use ...
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ژورنال
عنوان ژورنال: Journal of Vibroengineering
سال: 2016
ISSN: 1392-8716
DOI: 10.21595/jve.2016.16705