Design and mechanical testing of a variable stiffness morphing trailing edge flap-Reference-Cited by-同舟云学术

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Design and mechanical testing of a variable stiffness morphing trailing edge flap

Published:2017-07-28 Issue:4 Volume:29 Page:669-683
ISSN:1045-389X
Container-title:Journal of Intelligent Material Systems and Structures
language:en
Short-container-title:Journal of Intelligent Material Systems and Structures

Author:

Ai Qing¹,Weaver Paul M¹,Azarpeyvand Mahdi²³

Affiliation:

1. Advanced Composites Centre for Innovation and Science (ACCIS), Department of Aerospace Engineering, University of Bristol, Bristol, UK

2. Aeroacoustic and Aerodynamic Research Group (A2RG), University of Bristol, Bristol, UK

3. Department of Mechanical Engineering, University of Bristol, Bristol, UK

Funder

Engineering and Physical Sciences Research Council

Publisher

SAGE Publications

Subject

Mechanical Engineering,General Materials Science

Link

http://journals.sagepub.com/doi/pdf/10.1177/1045389X17721028

Reference46 articles.

1. Simplified analytical model for tapered sandwich beams using variable stiffness materials

2. Aerodynamic and aeroacoustic performance of airfoils with morphing structures

3. Experimental investigation of aerodynamic performance of airfoils fitted with morphing trailing edges

4. Design optimization of a morphing flap device using variable stiffness materials

5. Aeroelastic Considerations on Shape Control of an Adaptive Wing

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2. Time-Varying Aeroelastic Modeling and Analysis for a Morphing Wing;AIAA Journal;2024-07-27

3. Recent developments of polymer-based skins for morphing wing applications;Polymer Testing;2024-06

4. Mechanical properties and band gap characteristics of flexible skin based on multi-concave angle honeycomb;Materials Today Communications;2023-06

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