Membrane Micro Air Vehicles with Adaptive Aerodynamic Twist: Numerical Modeling-Reference-Cited by-同舟云学术

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Membrane Micro Air Vehicles with Adaptive Aerodynamic Twist: Numerical Modeling

Published:2007-04-23 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
language:
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Author:

Stanford Bret¹,Ifju Peter¹

Affiliation:

1. University of Florida

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-1758

Reference22 articles.

1. Profil und Auftrieb eines Segels

2. A Simple Model for Elastic Two-Dimensional Sails

3. Computational model of flexible membrane wings in steady laminar flow

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. Effect of Wing Flexibility on Lift and Thrust Production in Flapping Flight;AIAA Journal;2010-05

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