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Numerical Reproducing of a Bifurcation in the Stress Distribution Obtaining Process in Post-Critical Deformation States of Aircraft Load-Bearing Structures

机译：飞机承载结构后临界变形状态下应力分布中的分叉分叉的数值再现

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Tomasz Kopecki;
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年度 2012
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1. PROBLEMS OF NUMERICAL BIFURCATION REPRODUCING IN POST-CRITICAL DEFORMATION STATES OF AIRCRAFT STRUCTURES [J] . Tomasz Kopecki, Przemyslaw Mazurek Journal of teoretical and applied mechanics . 2013,第4期

机译：飞机结构临界变形后的数值分叉再现问题
2. POST-CRITICAL DEFORMATION STATES OF COMPOSITE THIN-WALLED AIRCRAFT LOAD-BEARING STRUCTURES [J] . Kopecki Tomasz, Bakunowicz Jerzy, Lis Tomasz Journal of teoretical and applied mechanics . 2016,第1期

机译：复合薄壁飞机承重结构的临界后变形状态
3. POST-CRITICAL DEFORMATION OF THIN-WALLED LOAD-BEARING AIRCRAFT STRUCTURE REPRESENTING FRAGMENT OF THE ONE-WAY TORSION BOX [J] . Tomasz Kopecki, Tomasz Lis, Przemys?aw Mazurek Advances in Science and Technology Research Journal . 2018,第3期

机译：单向扭力箱的薄壁承重飞机结构代表片段的临界后变形
4. Effect of stiffeners on nature of post-critical deformations of thin-walled composite aircraft structures: A combined numerical-experimental study [C] . Jerzy Bakunowicz, Tomasz Kopecki, Tomasz Lis, International Conference on Mechanical and Aerospace Engineering . 2016

机译：加劲肋对薄壁复合材料飞机结构临界变形后性质的影响：组合数值实验研究
5. Efficient numerical techniques for predicting process-induced stresses and deformations in composite structures. [D] . Arafath, Abdul Rahim Ahamed. 2007

机译：用于预测复合结构中过程引起的应力和变形的有效数值技术。
6. Numerical investigation of airborne contaminant transport under different vortex structures in the aircraft cabin [O] . Fei Li, Junjie Liu, Jianlin Ren, -1

机译：机舱内不同旋涡结构下空气污染物迁移的数值研究
7. POST-CRITICAL DEFORMATION OF THIN-WALLED LOAD-BEARING AIRCRAFT STRUCTURE REPRESENTING FRAGMENT OF THE ONE-WAY TORSION BOX [O] . Tomasz Kopecki, Tomasz Lis, Przemysław Mazurek 2018

机译：薄壁承载飞机结构的关键后变形代表单向扭转箱片段的碎片
8. A numerical method for the stress analysis of stiffened-shell structures under nonuniform temperature distributions [R] . Heldenfels, Richard R 1951

机译：非均匀温度分布下加筋壳结构应力分析的数值方法

Numerical Reproducing of a Bifurcation in the Stress Distribution Obtaining Process in Post-Critical Deformation States of Aircraft Load-Bearing Structures

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