Research on Nonlinear Deformation and Stability of an Advanced Aircraft Fuselage Composite Section under Pure Bending

V. K. Belov; L. P. Zheleznov; T. S. Ognyanova

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Research on Nonlinear Deformation and Stability of an Advanced Aircraft Fuselage Composite Section under Pure Bending

机译：纯弯曲下先进飞机机身复合段的非线性变形及稳定性研究

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The finite element algorithm developed by the authors has been used for solving the strength and stability problems of shells. The effect of deformation nonlinearity, stiffness of stringer set, shell thickness on critical loads has been determined.

机译：作者开发的有限元算法已被用于解决壳的强度和稳定性问题。确定了变形非线性，纵梁刚度刚度，壳体厚度对临界负荷的影响。

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来源
《Russian Aeronautics》 |2017年第4期|共9页
作者
V. K. Belov; L. P. Zheleznov; T. S. Ognyanova;
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作者单位

S. A. Chaplygin Aeronautical Research Institute (SibNIA);

S. A. Chaplygin Aeronautical Research Institute (SibNIA);

S. A. Chaplygin Aeronautical Research Institute (SibNIA);

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原文格式 PDF
正文语种 eng
中图分类航空;
关键词
noncircular cylindrical composite shells; discrete reinforcement; nonlinear deformation; stability; finite element method;

机译：非圆形圆柱形复合壳;离散加固;非线性变形;稳定性;有限元法;

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专利

1. Research on Nonlinear Deformation and Stability of an Advanced Aircraft Fuselage Composite Section under Pure Bending [J] . V. K. Belov, L. P. Zheleznov, T. S. Ognyanova Russian Aeronautics . 2017,第4期

机译：纯弯曲下先进飞机机身复合段的非线性变形及稳定性研究
2. Nonlinear Deformation and Stability of Discretely-Supported Egg-Shaped Cylindrical Composite Shells under Transversal Bending and Internal Pressure [J] . L. P. Zheleznov, V. V. Kabanov, D. V. Boiko Journal of Machinery Manufacture and Reliability . 2014,第6期

机译：横向弯曲和内压作用下离散支撑的卵形圆柱复合壳的非线性变形和稳定性
3. A refined quasi-3D hybrid-type higher order shear deformation theory for bending and Free vibration analysis of advanced composites beams [J] . Meradjah Mustapha, Bouakkaz Khaled, Zaoui Fatima Zohra, Wind & structures . 2018,第4期

机译：精细的准3D混合型高阶剪切变形理论，用于高级复合材料梁的弯曲和自由振动分析
4. Experimental Research on the Stability behavior of Composite Curved Stiffened Fuselage Panel under Four-Point-Bending load [C] . C Hao, C Y Nan, Y Z Bo International Conference on Advanced Electronic Materials, Computers and Materials Engineering . 2019

机译：四点弯曲载荷复合弯曲机身面板稳定行为的实验研究
5. Advanced nonlinear control: Robustness and stability with applications to aircraft flight control systems. [D] . Frye, Michael Takaichi. 2006

机译：先进的非线性控制：鲁棒性和稳定性，可应用于飞机飞行控制系统。
6. A Refined Simple First-Order Shear Deformation Theory for Static Bending and Free Vibration Analysis of Advanced Composite Plates [O] . Hoang Nam Nguyen, Tran Thi Hong, Pham Van Vinh, 2019

机译：精细的简单一阶剪切变形理论用于高级复合板的静态弯曲和自由振动分析
7. THE EXPERIMENTAL-THEORETICAL STUDY OF NONLINEAR DEFORMATION AND LOSS OF STABILITY IN SHELLS OF REVOLUTION LOADED IN BENDING [O] . V.G. Bazhenov, A.I. Kibets, M.V. Petrov, 2010

机译：弯曲中旋转壳壳中非线性变形和稳定性损失的实验论研究
8. Instability of Short Circular Cylindrical Laminated Composite Shells under Pure Bending [R] . Villhard, V. J. 1980

机译：纯弯曲下短圆柱层合板的不稳定性

Research on Nonlinear Deformation and Stability of an Advanced Aircraft Fuselage Composite Section under Pure Bending

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