## 留言板

 引用本文: 童贤鑫, B. 盖尔, K. 沃厄尔. 复合材料离散加筋曲板在压剪联合载荷作用下的屈曲分析[J]. 应用数学和力学, 1986, 7(4): 295-305.
X. X. Tong, B. Geier, K. Rohwer. Buckling Analysis of Discretely Stiffened Composite Curved Panels under Compression and Shear[J]. Applied Mathematics and Mechanics, 1986, 7(4): 295-305.
 Citation: X. X. Tong, B. Geier, K. Rohwer. Buckling Analysis of Discretely Stiffened Composite Curved Panels under Compression and Shear[J]. Applied Mathematics and Mechanics, 1986, 7(4): 295-305.

## Buckling Analysis of Discretely Stiffened Composite Curved Panels under Compression and Shear

• 摘要: 给出了一种复合材料加筋曲板压剪下的屈曲分析方法,分析中采用"板条有限元素法".文中针对复位移函数提出了一种改进方案,使运算可在实数范围内进行;还介绍了一种满足各类典型边界条件的简便处理方法.计算了一些实例,与现存的解符合较好.
•  [1] Seydel,E.,Beitrag zur Frags des Ausbeulens von Versteiften Platten bei Schubbeanspruchung,DVL-Bericht,Luftfahrforschung,8,3(1930).(Лехнипкий С.Г.,Анцзомропные Пласмцнкц,§104). [2] Viswanathan,A.V.,M.Tamkuni and L.L.Baker,Elastic stability of laminated,flat and curved,long rectangular plates subjected to combined inplane loads,NASA CR-2330,June(1974). [3] Viswanathan,A.V.,Soong Tsai-chen and R.E.Miller,Jr.,Buckling analysis for axially compressed flat plates,structural sections,and stiffened plates reinforced with laminated composites,NASA CR-1887,Nov.(1971). [4] Viswanathan,A.V.and M.Tamekuni,Elastic buckling analysis for composite stiffened panels and other structures subjected to biaxial inplane loads,NASA CR-2216,Sep.(1973). [5] Geier,B.,Introduction to the mechanics of composite laminates,IB,131-82/12(DFVLR). [6] Fan,S.F.,B.Geier,K.Rohwer and D.C.Liu,Stability of layered anisotropic cylindrical shells under combined loading,IB,131-83(DFVLR). [7] 童贤鑫,复合材料加筋迭层板的轴压稳定性分析,HJB84016,中国航空科技文献.

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##### 出版历程
• 收稿日期:  1985-05-09
• 刊出日期:  1986-04-15

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