Parametric Representation and Shape Optimization of a Wing for Flapping Micro Air Vehicles-Reference-Cited by-同舟云学术

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Parametric Representation and Shape Optimization of a Wing for Flapping Micro Air Vehicles

Published:2011-04-04 Issue: Volume: Page:
ISSN:
Container-title:52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
language:
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Author:

Stewart Eric¹,Patil Mayuresh¹,Canfield Robert¹,Snyder Richard²

Affiliation:

1. Virginia Polytechnic Institute and State University

2. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-2027

Reference29 articles.

1. Optimization of a Biplane Micro Air Vehicle

2. Insectlike Flapping Wings in the Hover Part II: Effect of Wing Geometry

3. 3Day, A. H., Optimization of a Micro Aerial Vehicle Planform Using Genetic Algorithms, M.s. thesis, Mechanical Engineering Dept.Worcester Polytechnic Institute, Worcester, MA,2007.

4. Shape, Structure, and Kinematic Parameterization of a Power-Optimal Hovering Wing

5. Falling Paper: Navier-Stokes Solutions, Model of Fluid Forces, and Center of Mass Elevation

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1. Design and Analysis of a Micro Class UAV Integrating Zimmerman Configuration;International Journal of Innovative Science and Research Technology (IJISRT);2024-03-29

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