Simply-Supported Saddle-Shaped Thick Symmetric Cross-Ply Panels: Full Surface-Parallel Boundary Constraints

Chaudhuri Reaz A.; Oktem A. Sinan

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Simply-Supported Saddle-Shaped Thick Symmetric Cross-Ply Panels: Full Surface-Parallel Boundary Constraints

机译：支撑简单的鞍形厚对称交叉面板：完全平行的边界约束

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来源
《AIAA Journal》 |2016年第7期|2191-2196|共6页
作者
Chaudhuri Reaz A.; Oktem A. Sinan;
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作者单位

Univ Utah, Dept Mat Sci & Engn, 122 S Cent Campus Dr,Room 304, Salt Lake City, UT 84112 USA;

Gebze Tech Univ, Dept Mech Engn, TR-41400 Kocaeli, Turkey;

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
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1. Analysis of Simply-Supported Saddle-Shaped Symmetric Cross-Ply Panels with No Surface-Parallel Boundary Constraints [J] . Chaudhuri Reaz A., Oktem A. Sinan AIAA Journal . 2016,第2期

机译：无表面平行边界约束的简支鞍形对称交叉板的分析
2. Flattening Effect of Negative Gaussian Curvature on Simply Supported Thick Asymmetric Cross-Ply Panels in the Absence of Surface-Parallel Edge Restraints [J] . Chaudhuri Reaz A., Oktem A. Sinan Journal of aerospace engineering . 2020,第6期

机译：阴性高斯曲率在缺失表面平行边缘限制的情况下简单地支撑厚的不对称交叉层面板的平坦化效应
3. Effect of boundary constraint on the frequency response of moderately thick doubly curved cross-ply panels using mixed fourier solution functions [J] . Chaudhuri RA, Kabir HRH Journal of Sound and Vibration . 2005,第1a2期

机译：边界约束对使用混合傅里叶解函数的中厚双曲交叉面板的频率响应的影响
4. A Semi- Energy Finite Strip Method for Post-Buckling Analysis of Relatively Thick Anti-Symmetric Cross-Ply Laminates [C] . Mohammad Hajikazemi, Hamid Reza Ovesy, Mohammad Homayoun Sadr ICCST8;International Conference on Composite Science and Technology . 2011

机译：相对厚的反对称交叉层板屈曲后分析的半能量有限条法
5. Three-dimensional boundary element analysis of residual stresses in a cross-ply fiber composite model. [D] . Lee, Sang Soon. 1992

机译：交叉纤维复合材料模型中残余应力的三维边界元分析。
6. Free Vibration Analysis of Closed Moderately Thick Cross-Ply Composite Laminated Cylindrical Shell with Arbitrary Boundary Conditions [O] . Dongyan Shi, Dongze He, Qingshan Wang, 2020

机译：具有任意边界条件的闭合中厚跨层复合层合圆柱壳的自由振动分析
7. Free Vibration Analysis of Closed Moderately Thick Cross-Ply Composite Laminated Cylindrical Shell with Arbitrary Boundary Conditions [O] . Dongyan Shi, Dongze He, Qingshan Wang, 2020

机译：具有任意边界条件的闭合中厚交叉帘布层复合圆柱形壳体的自由振动分析
8. EXPERIMENTAL INVESTIGATION OF THICK, AXIALLY SYMMETRIC BOUNDARY LAYERS ON CYLINDERS AT SUBSONIC AND HYPERSONIC SPEEDS [R] . Ronald L. Richmond 1957

机译：在超音速和超音速下圆柱上厚，轴对称边界层的实验研究

Simply-Supported Saddle-Shaped Thick Symmetric Cross-Ply Panels: Full Surface-Parallel Boundary Constraints

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