Parameterized Modeling Methodology for Efficient Aeroservoelastic Analysis of a Morphing Wing-Reference-Cited by-同舟云学术

Parameterized Modeling Methodology for Efficient Aeroservoelastic Analysis of a Morphing Wing

Published:2019-12 Issue:12 Volume:57 Page:5543-5552
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Huang Rui¹,Yang Zhijun¹,Yao Xiangjie¹,Zhao Yonghui¹,Hu Haiyan¹

Affiliation:

1. State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China

Funder

National Natural Science Foundation of China

Research Fund of State Key Laboratory of Mechanics and Control of Mechanical Structures

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference17 articles.

1. Aircraft Active Flutter Suppression: State of the Art and Technology Maturation Needs

2. Nonlinear Modal Aeroservoelastic Analysis Framework for Flexible Aircraft

3. Dynamic Aeroservoelastic Response with Nonlinear Structural Elements

4. A review of modelling and analysis of morphing wings

5. Morphing aircraft: The need for a new design philosophy

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