Deterministic Design Optimization of a Bendable Load Stiffened UAV Wing-Reference-Cited by-同舟云学术

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Deterministic Design Optimization of a Bendable Load Stiffened UAV Wing

Published:2010-01-04 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
language:
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Author:

Jagdale Vijay¹,Ifju Peter¹,Patil Abhishek¹,Stanford Bret¹

Affiliation:

1. University of Florida

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-1317

Reference25 articles.

1. Ifju et al. U.S.Patent "Bendable wing for micro air vehicle,"Patent no. : US7,331,546 B2DateofPatent: Feb.19,2008.

2. Multidisciplinary aerospace design optimization: survey of recent developments

3. Conceptual Design of a Bendable UAV Wing Considering Aerodynamic and Structural Performance

Cited by 3 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. Aeroelastic Shape Optimization of a Flapping Wing;Journal of Aircraft;2016-05

2. Parametric Representation and Shape Optimization of a Wing for Flapping Micro Air Vehicles;52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference;2011-04-04

3. Design Optimization of a Bendable UAV Wing Under Uncertainty;51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 18th AIAA/ASME/AHS Adaptive Structures Conference<BR> 12th;2010-04-12

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