Conceptual Design of a Bendable UAV Wing Considering Aerodynamic and Structural Performance-Reference-Cited by-同舟云学术

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

Published:2009-05-04 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
language:
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Author:

Jagdale Vijay¹,Stanford Bret¹,Ifju Peter¹,Patil Abhishek¹

Affiliation:

1. University of Florida

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-2641

Reference28 articles.

1. Development of a Composite Bendable-Wing Micro Air Vehicle

2. Multidisciplinary aerospace design optimization: survey of recent developments

3. Multidisciplinary Shape and Layup Optimization of a Bendable Composite UAV Wing

4. Modeling of Bendable MAV Wing Using Energy Method

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. A Study on Structural Dynamic Characteristics and Topology Optimization of Loitering Munition Under High Overloads;Lecture Notes in Mechanical Engineering;2024

2. 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

3. Deterministic Design Optimization of a Bendable Load Stiffened UAV Wing;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04

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