| 剪切锁闭的本质及解除方法 |
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| 引用本文： | 王寿梅,刘智勇.剪切锁闭的本质及解除方法[J].航空学报,1989,10(1):74-78. |
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| 作者姓名： | 王寿梅 刘智勇 |
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| 作者单位： | 北京航空航天大学
(王寿梅)，北京航空航天大学(刘智勇) |
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| 摘 要： | C0连续的弯曲单元得到了广泛应用,一方面由于计算较厚结构（如夹层结构）的需要,一方面由于在构造C1连续单元时遇到困难。但C0连续单元有“剪切锁团”问题,即当计算薄的结构时,剪切应变能愈来愈大,结构过分刚硬,位移很小。
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| 关 键 词： | 剪切锁闭 本质 解除 |
| 收稿时间： | 1987-10-07; |
THE ESSENCE AND ELIMINATION OF SHEAR LOCKING |
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| Beijing University of Aeronautics and Astronautics Wang Shoumei and Liu Zhiyong.THE ESSENCE AND ELIMINATION OF SHEAR LOCKING[J].Acta Aeronautica et Astronautica Sinica,1989,10(1):74-78. |
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| Authors: | Beijing University of Aeronautics and Astronautics Wang Shoumei and Liu Zhiyong |
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| Institution: | Beijing University of Aeronautics and Astronautics Wang Shoumei and Liu Zhiyong |
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| Abstract: | The paper tries to analyse the causation of shear locking for co-continuity bending elements, pointing out that the gross error of equilibrium in the elements is essential. Bulb functions and high order terms have been added to the shape functions to improve the equilibrium relationship but the total number of element D. O. F. was not increased. Numerical examples show that the shear locking is relieved. Hourglass'can be avoided because reduced integration is no longer needed. Also, accuracy deterioration when computing thick plates is removed. |
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| Keywords: | shear locking essence elimination |
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