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有限元软件在飞机结构打样设计中的应用 被引量:4
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作者 翟新康 黄其青 殷之平 《机械设计与制造》 北大核心 2007年第9期4-6,共3页
针对飞机结构打样设计阶段缺乏全机有限元模型,无法快速对结构进行初步强度估算,在工程梁理论的基础上,充分利用静力等效原则及圣维南原理,有效使用有限元软件,提出一种合理、快捷、高效的有限元力学建模方法。算例及大量的工程实际应... 针对飞机结构打样设计阶段缺乏全机有限元模型,无法快速对结构进行初步强度估算,在工程梁理论的基础上,充分利用静力等效原则及圣维南原理,有效使用有限元软件,提出一种合理、快捷、高效的有限元力学建模方法。算例及大量的工程实际应用表明:该方法效率高、实用性广,可以大大缩减飞机研制周期。 展开更多
关键词 打样设计 有限元模型 圣维南原理 工程梁理论
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Influence of residual stresses on failure pressure of cylindrical pressure vessels 被引量:4
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作者 M.Jeyakumar T.Christopher 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2013年第6期1415-1421,共7页
The utilization of pressure vessels in aerospace applications is manifold.In this work,fnite element analysis(FEA)has been carried out using ANSYS software package with 2D axisymmetric model to access the failure pr... The utilization of pressure vessels in aerospace applications is manifold.In this work,fnite element analysis(FEA)has been carried out using ANSYS software package with 2D axisymmetric model to access the failure pressure of cylindrical pressure vessel made of ASTM A36 carbon steel having weld-induced residual stresses.To fnd out the effect of residual stresses on failure pressure,frst an elasto-plastic analysis is performed to fnd out the failure pressure of pressure vessel not having residual stresses.Then a thermo-mechanical fnite element analysis is performed to assess the residual stresses developed in the pressure vessel during welding.Finally one more elasto-plastic analysis is performed to assess the effect of residual stresses on failure pressure of the pressure vessel having residual stresses.This analysis indicates reduction in the failure pressure due to unfavorable residual stresses. 展开更多
关键词 Aerospace engineering ASTM A36 Finite element analysis Pressure vessels Welding residual stress
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