Rapid wing structural finite element modeling and automated adjustment

被引：0

作者：

Luo, Mingqiang ^{[1
]}

Feng, Haocheng ^{[1
]}

Liu, Hu ^{[1
]}

Wu, Zhe ^{[1
]}

机构：

[1] School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

来源：

Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics | 2011年 / 37卷 / 06期

关键词：

D O I：

暂无

中图分类号：

学科分类号：

摘要：

引用

页码：680 / 684

共 50 条

[41] Interval finite element analysis of wing flutter
Institute of Solid Mechanics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
Chin J Aeronaut, 2008, 2 (134-140):
[42] Prediction of femoral fracture load using automated finite element modeling - Response
Keyak, JH
Rossi, SA
JOURNAL OF BIOMECHANICS, 2001, 34 (04) : 561 - 561
[43] Interval finite element analysis of wing flutter
Wang Xiaojun
Qiu Zhiping
CHINESE JOURNAL OF AERONAUTICS, 2008, 21 (02) : 134 - 140
[44] Finite element modeling
Markopoulos, Angelos P.
SpringerBriefs in Applied Sciences and Technology, 2013, 0 (9781447143291): : 29 - 57
[45] Finite element modeling
不详
R&D MAGAZINE, 2000, 42 (05): : 66 - 66
[46] Finite element modeling
Pasquet, Philippe
EUROPEAN JOURNAL OF COMPUTATIONAL MECHANICS, 2010, 19 (04): : 467 - 468
[47] Finite element modeling
SpringerBriefs in Applied Sciences and Technology, 2015, 21 : 53 - 57
[48] Finite element modeling
不详
R&D MAGAZINE, 2000, 42 (04): : 52 - 52
[49] Structural Design and Finite Element Analysis of Unfolding Process for All Composite Folding Wing of UAV
Lv, Peng
Lv, Shengli
Yang, Guangjun
Zeng, Qingna
Tong, Xiaoyan
ADVANCES IN STRUCTURES, PTS 1-5, 2011, 163-167 : 2328 - 2332
[50] Finite Element Analysis of an Aircraft Wing Leading Edge Made of GLARE Material for Structural Integrity
Shetty B.P.
Reddy S.
Mishra R.K.
Mishra, R.K. (rkmishra.drdo@gmail.com), 2017, Springer Science and Business Media, LLC (17) : 948 - 954