| THERMOELASTICITY ANALYSIS OF FINITE COMPOSITE LAMINATES WEAKENED BY MULTIPLE ELLIPTICAL HOLES |
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| 引用本文： | 许希武,孙良新,范绪箕. THERMOELASTICITY ANALYSIS OF FINITE COMPOSITE LAMINATES WEAKENED BY MULTIPLE ELLIPTICAL HOLES[J]. 应用数学和力学(英文版), 1995, 16(3): 257-267. DOI: 10.1007/BF02450526 |
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| 作者姓名： | 许希武 孙良新 范绪箕 |
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| 基金项目： | Project supported by the Aeronautics Science Foundation of China |
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| 摘 要： | ＴＨＥＲＭＯＥＬＡＳＴＩＣＩＴＹＡＮＡＬＹＳＩＳＯＦＦＩＮＩＴＥＣＯＭＰＯＳＩＴＥＬＡＭＩＮＡＴＥＳＷＥＡＫＥＮＥＤＢＹＭＵＬＴＩＰＬＥＥＬＬＩＰＴＩＣＡＬＨＯＬＥＳＸｕＸｉ－ｗｕ（许希武）ＳｕｎＬｉａｎｇ－ｘｉｎ（孙良新）ＦａｎＸｕ－ｑｉ（范绪箕）...
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| 收稿时间： | 1993-11-22 |
Thermoelasticity analysis of finite composite laminates weakened by multiple elliptical holes |
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| Xu Xi-wu,Sun Liang-xin,Fan Xu-qi. Thermoelasticity analysis of finite composite laminates weakened by multiple elliptical holes[J]. Applied Mathematics and Mechanics(English Edition), 1995, 16(3): 257-267. DOI: 10.1007/BF02450526 |
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| Authors: | Xu Xi-wu Sun Liang-xin Fan Xu-qi |
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| Affiliation: | Department of Aircraft, Nanjing University, of Aeronautics & Asironautics, Nanjing 210016 |
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| Abstract: | A finite composite laminate weakened by multiple elliptical holes of arbitrarydistribution, arbitrary orientation and arbitrary dimension, is treated as an anisotropic,finite multiple connected thin plate. Using the complex potential method in planetheory of heat conduction and elastictiy of an anisotropic body, the analytical solutionof a finite composite laminated plate subjected io arbitrary mechanical and thermalloads with multiple elliptical holes is. obtained by means of the Faber series expansion,mapping and the least square boundary collocation technique. The effects of someparameters on the thermostress distribution are studied in detail. Some conclusions aredrawn. |
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| Keywords: | composite laminates.heat conduction. thermoelasticity stressconcentration. holes |
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