Shape Optimization of a Membrane Wing for Micro Air Vehicles-Reference-Cited by-同舟云学术

Shape Optimization of a Membrane Wing for Micro Air Vehicles

Published:2004-02 Issue:2 Volume:42 Page:424-426
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Lian Yongsheng¹,Shyy Wei¹,Haftka Raphael T.¹

Affiliation:

1. University of Florida, Gainesville, Florida 32611

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.9106

Reference12 articles.

1. Flapping and flexible wings for biological and micro air vehicles

2. Flexible-wing-based micro air vehicles

3. 3Shyy, W., Udaykumar, H. S., Rao, M. M., and Smith, R. W., Computational Fluid Dynamics with Moving Boundaries, Taylor and Francis, Philadelphia, 1996, pp.31, 32.

4. Numerical analysis of three-dimensional elastic membrane wings

5. Membrane Wing Model for Micro Air Vehicles

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