Design and experiment of concentrated flexibility-based variable camber morphing wing-Reference-Cited by-同舟云学术

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Design and experiment of concentrated flexibility-based variable camber morphing wing

Published:2021-05 Issue: Volume: Page:
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

LI Yuzhu,GE Wenjie,ZHOU Jin,ZHANG Yonghong,ZHAO Donglai,WANG Zhuo,DONG Dianbiao

Funder

National Natural Science Foundation of China

Natural Science Foundation of Shaanxi Province

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference47 articles.

1. Three-dimensional design of a large-displacement morphing wing droop nose device;Vasista;J Intell Mater Syst Struct,2018

2. A review of morphing aircraft;Barbarino;J Intell Mater Syst Struct,2011

3. Realization of morphing wings: a multidisciplinary challenge;Vasista;J Aircraft,2012

4. SMA-actuated morphing wing with varying spanwise curvature and swept angle;Wang,2019

5. Performance of a three-dimensional morphing wing and comparison with a conventional wing;Previtali;AIAA J,2014

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1. Nonlinear fluid-solid coupling responses of flexible skin-based morphing camber wings;International Journal of Mechanical Sciences;2024-09

2. Design optimization and testing of a morphing leading-edge with a variable-thickness compliant skin and a closed-chain mechanism;CHINESE J AERONAUT;2024

3. Aerodynamic characteristics of a pitching airfoil with leading-edge morphing;Chinese Journal of Aeronautics;2024-07

4. Design optimization and testing of a morphing leading-edge with a variable-thickness compliant skin and a closed-chain mechanism;Chinese Journal of Aeronautics;2024-07

5. Structural Analysis and Testing of a Flexible Rudder Using a Cosine Honeycomb Structure;Aerospace;2024-06-08

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