Static analysis of shear-deformable aircraft wings using a multilayered functionally graded material model-Reference-Cited by-同舟云学术

Static analysis of shear-deformable aircraft wings using a multilayered functionally graded material model

Published:2023-10-30 Issue: Volume: Page:1-25
ISSN:0924-3046
Container-title:Advanced Composite Materials
language:en
Short-container-title:Advanced Composite Materials

Author:

Kim Dong-Hyeop¹²,Amir Mohammad²,Kim Sang-Woo¹²

Affiliation:

1. School of Aerospace and Mechanical Engineering, Korea Aerospace University 10540, Goyang-si, Gyeonggi-do, Republic of Korea

2. Research Institute for Aerospace Engineering and Technology, Korea Aerospace University 10540, Goyang-si, Gyeonggi-do, Republic of Korea

Funder

National Research Foundation of Korea

Publisher

Informa UK Limited

Subject

Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Link

https://www.tandfonline.com/doi/pdf/10.1080/09243046.2023.2274203

Reference49 articles.

1. Transient Response of a Single Degree-of-Freedom Wing at High Angle-of-Attack

2. Miglani J Zhao W Desai S et al. Analysis design and experiments of metal flat plate and foam airfoil flutter test articles. AIAA Scitech 2021 Forum. 2021; 1497.

3. Investigation of Aluminum and composite aircraft wings under the Influence of Aerodynamic Forces and their effects on environmental impacts;Ebadi S;J Environ Friendly Manage,2021

4. Vibration analysis of composite airfoil blade using orthotropic thin shell bending theory

5. Manufacturing ZrB2–SiC–TaC Composite: Potential Application for Aircraft Wing Assessed by Frequency Analysis through Finite Element Model

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