Optimal Design of a Seamless Aeroelastic Wing Structure-Reference-Cited by-同舟云学术

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Optimal Design of a Seamless Aeroelastic Wing Structure

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:

Perera Melanie¹,Guo Shijun¹

Affiliation:

1. Cranfield University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-2195

Reference38 articles.

1. Power Systems and Requirements for Integration of Smart Structures into Aircraft

2. Free vibration analysis of anisotropic thin-walled closed-section beams

3. Coupled bending-torsional dynamic stiffness matrix for timoshenko beam elements

4. Free vibration of composite beams - An exact method using symbolic computation

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1. Structural design and optimization of a morphing wing trailing edge flap;Aerospace Systems;2018-11-13

2. Morphing structures and fatigue: The case of an unmanned aerial vehicle wing leading edge;Fatigue & Fracture of Engineering Materials & Structures;2017-07-12

3. Controllability Analysis of Flexible Variable Sweep Control Wing;Advanced Materials Research;2012-06

4. Trim Optimizations of an Adaptive Tailless Aircraft with Composite Wing;Advanced Materials Research;2011-02

5. A Composite Wing Structure with a Morphing Leading Edge;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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