Stress Analysis of Membrane Flapping-Wing Aerial Vehicle Based on Different Material Models

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ISSN Print: 2327-4352
ISSN Online: 2327-4379
www.scirp.org/journal/jamp
E-mail: jamp@scirp.org

"Stress Analysis of Membrane Flapping-Wing Aerial Vehicle Based on Different Material Models"
written by Chunjin Yu, Daewon Kim, Yi Zhao,
published by Journal of Applied Mathematics and Physics, Vol.2 No.12, 2014

has been cited by the following article(s):

[1]	Research on Altitude Control of Flapping-Wing Aircraft Based on Nonlinear Backstepping Method
	… on Robotics & …, 2023

[2]	Conceptual design and parametric structural modeling of a FWAV biomimetic flapping wing
	2021

[3]	Fibrous Orientation Effects on the Deformation and Stress of a Pigeon-like Flapping-wing Micro Aerial Vehicle Based on APDL
	2020

[4]	Fibrous Orientation Effects on the Deformation and Stress of an Insect-like Flapping-wing Micro Aerial Vehicle Based on ACP
	2019

[5]	Numerical Analysis of the Influence of Fibre Orientations in a two-layered Biomimetic Flapping Wing
	2017 International Conference on Mechanical, Material and Aerospace Engineering (2MAE 2017), 2017

[1]	Research on Altitude Control of Flapping-Wing Aircraft Based on Nonlinear Backstepping Method 2023 5th International Symposium on Robotics & Intelligent Manufacturing Technology (ISRIMT), 2023 DOI:10.1109/ISRIMT59937.2023.10428450

[2]	Conceptual design and parametric structural modeling of a FWAV biomimetic flapping wing IOP Conference Series: Materials Science and Engineering, 2021 DOI:10.1088/1757-899X/1024/1/012015

[3]	Fibrous Orientation Effects on the Deformation and Stress of a Pigeon-like Flapping-wing Micro Aerial Vehicle Based on APDL IOP Conference Series: Materials Science and Engineering, 2020 DOI:10.1088/1757-899X/816/1/012002

[4]	Fibrous Orientation Effects on the Deformation and Stress of an Insect-like Flapping-wing Micro Aerial Vehicle Based on ACP IOP Conference Series: Materials Science and Engineering, 2019 DOI:10.1088/1757-899X/585/1/012060

[5]	Numerical Analysis of the Influence of Fibre Orientations in a two-layered Biomimetic Flapping Wing MATEC Web of Conferences, 2017 DOI:10.1051/matecconf/201711403005

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