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A STUDY OF THE EFFECT OF INITIAL IN-PLANE STRESSES ON VIBRATION AND BUCKLING BEHAVIOUR OF DAMPED COMPOSITE SANDWICH PLATES

机译：初始面内应力对阻尼复合三明治板振动和屈曲行为的影响研究

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Two new C° assumed strain finite element formulations of Reddy's higher-order theory are used to determine the effects of initial stresses on the natural frequencies and stability response of damped composite sandwich plates. Several parametric studies are presented to show the effects of length to thickness ratio, boundary conditions and lamination scheme on the vibration and stability of initially stressed damped composite sandwich plates.

机译：两个新的C°假设的Reddy高阶理论的菌株有限元制剂用于确定初始应力对阻尼复合夹层板的自然频率和稳定性响应的影响。提出了几项参数研究以显示长度与厚度比，边界条件和层压方案对初始应力阻尼复合夹层板的振动和稳定性的影响。

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《International conference on sandwich structures》|2003年||共10页
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Ajaya K. Nayak; Stuart S. J. Moy; R. Ajit Shenoi;
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中图分类工程材料一般性问题;
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1. Assumed Strain Finite Elements for Buckling and Vibration Analysis of Initially Stressed Damped Composite Sandwich Plates [J] . A. K. Nayak, R. A. Shenoi Journal of Sandwich Structures and Materials . 2005,第4期

机译：假设屈曲和振动分析最初应力阻尼复合夹层板的屈曲和振动分析的应变有限元
2. Vibration of cross-ply laminated composite plates subjected to initial in-plane stresses [J] . Hiroyuki Matsunaga Thin-Walled Structures . 2002,第7a8期

机译：承受初始面内应力的交叉层压复合板的振动
3. Active constrained layer damping of geometrically nonlinear vibrations of smart laminated composite sandwich plates using 1-3 piezoelectric composites [J] . R. Suresh Kumar, M. C. Ray International journal of mechanics and materials in design . 2012,第4期

机译：使用1-3压电复合材料的智能层合夹层板几何非线性振动的主动约束层阻尼。
4. A STUDY OF THE EFFECT OF INITIAL IN-PLANE STRESSES ON VIBRATION AND BUCKLING BEHAVIOUR OF DAMPED COMPOSITE SANDWICH PLATES [C] . Ajaya K. Nayak, Stuart S. J. Moy, R. Ajit Shenoi International conference on sandwich structures . 2003

机译：初始面内应力对阻尼复合三明治板振动和屈曲行为的影响研究
5. Free vibration and buckling analysis of thin rectangular plates with classical boundary conditions under unilateral in-plane loads. [D] . Michelussi, David J. 1997

机译：单边面内载荷下具有经典边界条件的矩形薄板的自由振动和屈曲分析。
6. Multiscale studies on the nonlinear vibration of delaminated composite laminates–global vibration mode with micro buckles on the interfaces [O] . Jianghong Xue, Fei Xia, Jun Ye, -1

机译：分层复合材料层合板非线性振动的多尺度研究–界面处带有微扣的整体振动模式
7. Exact Solutions for Vibration and Buckling of An SS-C-SS-C Rectangular Plate Loaded by Linearly Varying In-plane Stresse [O] . 2004

机译：通过线性变化的平面内应力加载SS-C-SS-C矩形板的振动和屈曲的精确解决方案
8. User manual for VICONOPT: An exact analysis and optimum design program covering the buckling and vibration of prismatic assemblies of flat in-plane loaded, anisotropic plates, with approximations for discrete supports, and transverse stiffeners [R] . Williams, F. W., Anderson, M. S., Kennedy, D., 1990

机译：VICONOpT的用户手册：精确分析和优化设计程序，涵盖扁平面内加载各向异性板的棱柱组件的屈曲和振动，近似于离散支撑和横向加强筋

A STUDY OF THE EFFECT OF INITIAL IN-PLANE STRESSES ON VIBRATION AND BUCKLING BEHAVIOUR OF DAMPED COMPOSITE SANDWICH PLATES

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