Nonlinear Aeroelastic Study for Folding Wing Structures

Author:

Attar Peter J.1,Tang Deman2,Dowell Earl H.2

Affiliation:

1. University of Oklahoma, Norman, Oklahoma 73019

2. Duke University, Durham, North Carolina 27708-0300

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 45 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. Supersonic flutter mechanism of “diamond-back” folding wings;Aerospace Science and Technology;2024-10

2. Flutter Characteristics of a Modified Z-Shaped Folding Wing Using a New Non-Intrusive Model;Aerospace;2024-05-24

3. Nonlinear Aeroelastic Response Analysis of Wing with Flared Folding Wingtip;Journal of Aerospace Engineering;2024-05

4. Approximate global mode method for flutter analysis of folding wings;International Journal of Mechanical Sciences;2024-03

5. Aeroelasticity Analysis of Folding Wing with Structural Nonlinearity Using Modified DLM;Revista Internacional de Métodos Numéricos para Cálculo y Diseño en Ingeniería;2024

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