Supersonic Flutter and Buckling Optimization of Tow-Steered Composite Plates-Reference-Cited by-同舟云学术

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Supersonic Flutter and Buckling Optimization of Tow-Steered Composite Plates

Published:2019-01 Issue:1 Volume:57 Page:397-407
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Guimarães Thiago A. M.¹,Castro Saullo G. P.²,Cesnik Carlos E. S.³,Rade Domingos A.⁴

Affiliation:

1. Federal University of Uberlândia, 38408-100 Uberlândia, Brazil

2. Delft University of Technology, 2629 HS Delft, The Netherlands

3. University of Michigan, Ann Arbor, Michigan 48109-2140

4. Aeronautics Institute of Technology, 12228-900 São José dos Campos, Brazil

Funder

Conselho Nacional de Desenvolvimento Científico e Tecnológico

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J057282

Reference32 articles.

1. Nonlinear oscillations of a fluttering plate.

2. Panel flutter - A review of the aeroelastic stability of plates and shells

3. Finite-element panel flutter in three-dimensional supersonic unsteady potential flow

4. Finite element nonlinear panel flutter with arbitrary temperatures in supersonic flow

5. Finite element method for large-amplitude two-dimensional panel flutter at hypersonic speeds

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2. Active aeroelastic flutter control of supersonic smart variable stiffness composite panels using layerwise models;Composite Structures;2024-09

3. Nonlinear thermal flutter of variable angle tow composite laminates in supersonic airflow;Mechanics of Advanced Materials and Structures;2024-07-31

4. Exploring the nonlinear response of cracked variable stiffness composite plates using plate decomposition method;Composite Structures;2024-06

5. Layerwise models for supersonic flutter analysis of viscoelastic sandwich panels with curvilinear fibre composite skins;Journal of Sound and Vibration;2024-03

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