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TEST AND ANALYSIS OF A COMPOSITE MULTI-BAY FUSELAGE PANEL UNDER UNI-AXIAL COMPRESSION

机译：单轴压缩下复合多层保温板的试验与分析

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Jian Li;
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年度 2008
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1. The computational post buckling analysis of fuselage stiffened panels loaded in compression [J] . C. Lynch, A. Murphy, M. Price, Thin-Walled Structures . 2004,第10期

机译：压缩加载的机身加筋板的计算后屈曲分析
2. The computational post buckling analysis of fuselage stiffened panels loaded in compression [J] . C. Lynch, A. Murphy, M. Price, Thin-Walled Structures . 2004,第10期

机译：压缩加载的机身加筋板的计算后屈曲分析
3. The computational post buckling analysis of fuselage stiffened panels loaded in compression [J] . C. Lynch, A. Murphy, M. Price, Thin-Walled Structures . 2004,第10期

机译：压缩加载机身加强面板的计算后屈曲分析
4. Test and Analysis of a Composite Multi- bay Fuselage Panel Under Uni- axial Compression [C] . J. Li, D. Baker AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference;AIAA Non-Deterministic Approaches Forum;AIAA/ASME/AHS Adaptive Structures Conference;AIAA Gossamer Spacecraft Forum . 2004

机译：复合材料多机架机身面板在单轴压缩下的测试与分析
5. Buckling and postbuckling analysis of stiffened composite panels in axial compression. [D] . Park, Oung. 1999

机译：加筋复合板在轴向压缩下的屈曲和屈曲后分析。
6. Effects of Reorientation of Graphene Platelets (GPLs) on Young’s Modulus of Polymer Nanocomposites under Uni-Axial Stretching [O] . Chuang Feng, Yu Wang, Sritawat Kitipornchai, 2017

机译：单轴拉伸下石墨烯血小板（GPLs）的取向对聚合物纳米复合材料杨氏模量的影响
7. The Computational Post Buckling Analysis Of Fuselage Stiffened Panels Loaded In Compression [O] . Lynch C., Murphy Adrian, Price Mark, 2004

机译：压缩加载的机身加筋板的计算后屈曲分析
8. Experimental Results From Stitched Composite Multi-Bay Fuselage Panels Tested Under Uni-Axial Compression [R] . Baker, Donald J. 2004

机译：单轴压缩下缝合复合多湾机身板的实验结果

TEST AND ANALYSIS OF A COMPOSITE MULTI-BAY FUSELAGE PANEL UNDER UNI-AXIAL COMPRESSION

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