scholarly journals Parametric study of composite wing box for high altitude platform using finite element analysis

2021 ◽  
Vol 1137 (1) ◽  
pp. 012018
Author(s):  
Nontawat Thaiprayoon ◽  
Kittigorn Chalernphon ◽  
Chompunut Somtua ◽  
Panya Aroonjarattham
2010 ◽  
Vol 163-167 ◽  
pp. 2328-2332 ◽  
Author(s):  
Peng Lv ◽  
Sheng Li Lv ◽  
Guang Jun Yang ◽  
Qing Na Zeng ◽  
Xiao Yan Tong

This paper discusses the unfolding form of the folding wing and its application to special UAV. The main investigations involve aspects such as unfolding process of the special UAV’s folding wing, contour structure of the complete unfolding, the choice of composite materials for the folding wing and its overall performance parameters. Modeling and dynamics analysis are made for all-composite wing through finite element analysis and calculating software. The unfolding process is also simulated. The result shows that the wing’s first-order frequency is low, second-order frequency and third-order frequency are close at different sweep angles. The wings are apt to happen flutter coupling in flutter analysis. With the continued folding of the wing, the wing’s natural frequency decreases significantly at different orders. The conclusions can provide effective basis for the study of wing rotational rate, unfolding time and impact action.


2014 ◽  
Vol 681 ◽  
pp. 222-228
Author(s):  
Shou Tao Yao ◽  
Wei Cheng Zhao ◽  
Qun Cheng

High-rise super large aerial platform project construction has been a greater danger, How to ensure the quality of components assembled and the safety of the construction project is worthy of study. Through finite element analysis on construction conditions of steel structures, ensures the hydraulic synchronous lifting and construction technology of high-altitude hoisting and assembly, greatly reduced the difficulty of installation, quality, safety, cost, schedule is guaranteed.


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