Aeroelastic Analysis of Spanwise Morphing Wing with Multistable Honeycomb-Reference-Cited by-同舟云学术

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Aeroelastic Analysis of Spanwise Morphing Wing with Multistable Honeycomb

Published:2022-01-03 Issue: Volume: Page:
ISSN:
Container-title:AIAA SCITECH 2022 Forum
language:
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Author:

Boston David M.¹,Phillips Francis R.²,Henry Todd³,Arrieta Andres F.¹

Affiliation:

1. Purdue University

2. US Army Research Laboratory Weapons and Materials Research Directorate

3. US Army Research Laboratory Weapons and Materials Research Directorate, US Army Research Laboratory Weapons and Materials Research Directorate, Aberdeen Proving Ground, MD, US, academic/mil

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0319

Reference23 articles.

1. Handbook of Compliant Mechanisms

2. Span Morphing: A Conceptual Design Study

3. A Mathematical Model for Roll Dynamics by Use of a Morphing-Span Wing

4. Morphing Aircraft Systems: Historical Perspectives and Future Challenges

Cited by 2 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 Analysis of Adaptive Small Unmanned Aerial System Wings;AIAA SCITECH 2024 Forum;2024-01-04

2. Homogenization Model for Multistable Honeycomb Metastructures Exhibiting Beam-like Behavior;AIAA SCITECH 2023 Forum;2023-01-19

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