CLC number: V22
On-line Access: 2024-08-27
Received: 2023-10-17
Revision Accepted: 2024-05-08
Crosschecked: 2019-09-02
Cited: 0
Clicked: 6120
Yu-shan Meng, Li Yan, Wei Huang, Tian-tian Zhang, Zhao-bo Du. Structural design and analysis of a composite wing with high aspect ratio[J]. Journal of Zhejiang University Science A, 2019, 20(10): 781-793.
@article{title="Structural design and analysis of a composite wing with high aspect ratio",
author="Yu-shan Meng, Li Yan, Wei Huang, Tian-tian Zhang, Zhao-bo Du",
journal="Journal of Zhejiang University Science A",
volume="20",
number="10",
pages="781-793",
year="2019",
publisher="Zhejiang University Press & Springer",
doi="10.1631/jzus.A1900271"
}
%0 Journal Article
%T Structural design and analysis of a composite wing with high aspect ratio
%A Yu-shan Meng
%A Li Yan
%A Wei Huang
%A Tian-tian Zhang
%A Zhao-bo Du
%J Journal of Zhejiang University SCIENCE A
%V 20
%N 10
%P 781-793
%@ 1673-565X
%D 2019
%I Zhejiang University Press & Springer
%DOI 10.1631/jzus.A1900271
TY - JOUR
T1 - Structural design and analysis of a composite wing with high aspect ratio
A1 - Yu-shan Meng
A1 - Li Yan
A1 - Wei Huang
A1 - Tian-tian Zhang
A1 - Zhao-bo Du
J0 - Journal of Zhejiang University Science A
VL - 20
IS - 10
SP - 781
EP - 793
%@ 1673-565X
Y1 - 2019
PB - Zhejiang University Press & Springer
ER -
DOI - 10.1631/jzus.A1900271
Abstract: Wings with large aspect ratio have large bending moment and torque, so the poor flexural and torsional stiffness are noteworthy. The application of composite materials in wing structure can improve the performance of wing. In the design process of the wing with high aspect ratio, the design parameters of the wing are preliminarily set. Then, the wing configuration is determined according to the force characteristics referring to the indexes of the Predator unmanned aerial vehicle (UAV), and on the basis of the composite material mechanics and finite element theory, the finite element model of the wing is designed as well. Next, we carry out the aerodynamic analysis in FLUENT. At last, we use ANSYS composite Pre/Post (ACP) module to establish the static analysis of the wing, and two improvement schemes are proposed to deal with the problem that the wing with high aspect ratio would encounter.
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