Buckling test and optimum design of fiber reinforced composite plates under compression

In this paper, the conclusion that the experimental results coincide with theoretical analysis has been got through buckling test of 283 composite rectangular plates. It is confirmed that the critical loads of composite plates calculated by buckling theoretical formula of anisotropic plate are reliable. The selections of optimal content of matrix and optimal off-axis which make fiber reinforced composite plates reach biggest critical loads are also discussed in this paper. The result of analysis may be used in the design for the products.     

纤维增强复合材料矩形薄板压缩稳定试验及最优设计

本文通过283块玻璃钢矩形薄板的稳定试验,得出试验结果与理论分析一致的结论,证实按各向异性板的屈曲理论公式计算纤维增强复合材料薄板稳定临界载荷是可靠的.本文也给出了各种纤维增强复合材料薄板达到最大临界载荷的最优基体含量和最优偏角的选择,得出的结果可供产品设计时使用.     

ENDOCHRONIC ANALYSIS FOR COMPRESSIVE BUCKLING OF THIN－WALLED CYLINDERS IN YIELD REGION

ＥＮＤＯＣＨＲＯＮＩＣＡＮＡＬＹＳＩＳＦＯＲＣＯＭＰＲＥＳＳＩＶＥＢＵＣＫＬＩＮＧＯＦＴＨＩＮ－ＷＡＬＬＥＤＣＹＬＩＮＤＥＲＳＩＮＹＩＥＬＤＲＥＧＩＯＮＰｅｎｇＸｉａｎｇｈｅ（彭向和）ＣｈｅｎＹｕａｎｑｉａｎｇ（陈元强）ＺｅｎｇＸｉａｎｇｇｕｏ（曾祥...     

Creep buckling of cross-ply symmetric laminated cylindrical panels

A creep buckling analysis of cross-ply symmetric laminated cylindrical panels is given in this paper.By means of theoretical analysis,a method to determine the critical load of creep buckling of the panels with simply supported boundary conditons is obtained.     

确定薄板在二重特征值处屈曲状态的一种方法*

本文结合有限元法和摄动法给出了一个确定薄板在二重特征值处分支方向的方法.用此方法,我们对双向受压矩形板在二重特征值处的屈曲状态进行了数值计算,结果表明此方法是可行的.     

Numerical simulation of viscous flow: Buckling of planar jets

The phenomenon of viscous fluid buckling has a long and distinguished history, dating back to Taylor (1968). This paper is concerned with demonstrating that a numerical method, GENSMAC, is capable of simulating this physical instability. A table of the parameter values (e.g. the Reynolds number, the Froude number, inlet width, inlet velocity and aspect ratio) is provided giving details of when buckling occurs and when it does not. This allows the deduction of a possible buckling condition in terms of the Reynolds number and the ratio of height of the jet to the inlet width, modifying a previous hypothesis. Visualization of jet buckling is provided. This work has been motivated by the need of industry to understand jet filling of containers; jet buckling can lead to air entrapment and this is undesirable. Copyright © 1999 John Wiley & Sons, Ltd.     

The Crystal and Molecular Structure of 1,8-Dioxo-9- (o-nitrophenyl)-1,2,3,4,5,6,7,8-octahydroxanthene

The crystal structure of the title compound is described. The compound crystallizes in monoclinic space group P21/a with Z=4. The unit cell dimensions are a = 10.809(2), b = 9.998(2) and c = 14.855(3) Å, V = 1592(1) ų, D_cal = 1.399 g/cm³. The central ring of the octahydroxanthene moiety is slightly folded and the two outer rings are in sofa conformations. Due to the p-conjugation there is an electron delocalized stretch. The phenyl ring of the 2-nitrophenyl substituent is perpendicular to the octahydroxanthene ring system.