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Skin, Stringer, And Fastener Loads In Buckled Fuselage Panels

机译：带扣式机身面板中的皮肤，纵梁和紧固件负载

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Richard D. Young; Cheryl A. Rose; James H. Starnes Jr;
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年度 2001
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1. Critical buckling load of honeycomb sandwich panels reinforced by three- phase orthotropic skins enhanced by carbon nanotubes [J] . Composite Structures . 2020,第Apra期

机译：碳纳米管增强的三相正交各向异性蒙皮增强的蜂窝夹芯板的临界屈曲载荷
2. Buckling and Fracture Analysis of Composite Skin-Stringer Panel Using VCCT and FEA Software [J] . NASA Tech Briefs . 2006,第3期

机译：使用VCCT和FEA软件的复合纵梁面板的屈曲和断裂分析
3. Damage influence on the buckling load of CFRP stringer-stiffened panels [J] . M. Gaedke, B. Geier, H. -Chr. Goetting, Composite Structures . 1996,第3a4期

机译：损伤对CFRP桁条加劲板屈曲载荷的影响
4. Research on Buckling and Post-buckling Characteristics of Composite Curved Stiffened Fuselage Panel under Hoop Bending load [C] . C Hao, C Y Nan, Z Peng International Conference on Modeling in Mechanics and Materials . 2019

机译：箍弯载下复合弯曲加强机身面板屈曲和后屈曲特性研究
5. A cost of quality comparison analysis between manual assembly and automated assembly methods of fuselage skin panels [D] . Rose, Ron S. 1999

机译：机身蒙皮面板手动组装和自动组装方法之间的质量比较分析成本
6. Cross-Influence between Intra-Laminar Damages and Fibre Bridging at the Skin–Stringer Interface in Stiffened Composite Panels under Compression [O] . Angela Russo, Andrea Sellitto, Salvatore Saputo, 2019

机译：层压复合板在压缩状态下层内损伤与皮肤纵梁界面处的纤维桥接之间的交叉影响
7. Skin, Stringer, and Fastener Loads in Buckled Fuselage Panels [O] . Rose Cheryl A., Starnes James H. Jr., Young Richard D. 2001

机译：扭曲的机身面板中的蒙皮，纵梁和紧固件负载
8. Skin, Stringer, and Fastener Loads in Buckled Fuselage Panels [R] . Young, R. D. , Rose, C. A. , Starnes, J. H. 2001

机译：带扣机身面板中的蒙皮，纵梁和紧固件负载

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