Experimental and Finite Element Modal Analysis of a Pliant Membrane for Micro Air Vehicles Wings-Reference-Cited by-同舟云学术

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Experimental and Finite Element Modal Analysis of a Pliant Membrane for Micro Air Vehicles Wings

Published:2010-04-12 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 18th AIAA/ASME/AHS Adaptive Structures Conference<BR> 12th
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Author:

Albertani Roberto,Chakravarty Uttam

Publisher

American Institute of Aeronautics and Astronautics

Reference25 articles.

1. Mechanization and Control Concepts for Biologically Inspired Micro Air Vehicles

2. Laminar-Turbulent Transition of a Low Reynolds Number Rigid or Flexible Airfoil

3. Unsteady aerodynamics and flow control for flapping wing flyers

4. The added mass of a flexible plate oscillating in a fluid

5. Noca, F. "Apparent mass in viscous,vortical flows,"American Physical Society, 54th Annual Meeting of the Division of Fluid Dynamics, San Diego, California,Nov.2001.

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Nonlinear vibrations and instabilities of a stretched hyperelastic annular membrane;International Journal of Solids and Structures;2012-02

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