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1.
温度和加载速率影响位错发射的分子动力学模拟   总被引:2,自引:2,他引:0  
以A1作为研究对象,采用EAM势进行分子动力学模拟,在Ⅰ型和Ⅱ型加载条件下,研究了温度和取向对发射位错的临界应力强度因子的影响,模拟结果表明,裂尖发射位错的监介应力强度因子随温度升高指数规律降低,但却随加载速率的增大而升高。  相似文献   

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GEOMETRICFRAMEWORKANDMINIMALREALIZATIONSOFNONLINEARSYSTEMSONFIBREBUNDLEMuXiaowu(慕小武)(DepartmentofMathematics,ZhengzhouUnivers...  相似文献   

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NONLINEARTHREE-DIMENSIONALANALYSISOFCOMPOSITELAMINATEDPLATES¥(江晓禹,张相周,陈百屏)JiangXiaoyu;(SouthwesternJiaotongUniversity,Chengdu6...  相似文献   

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KANE’SEQUATIONSFORPERCUSSIONMOTIONOFVARIABLEMASSNONHOLONOMICMECHANICALSYSTEMSZhangYueliang(张耀良)(HarbinEngineeringUniversity,H...  相似文献   

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THEHAMILTONIANSTBUCTURESOF3DODEWITHTIME-INDEPENDENTINVARIANTSGuoZhong-heng(郭仲衡)(DepartmentofMathematics,PekingUniversity,Beij...  相似文献   

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ANEWMETHODFORTHECONSTRUCTIONOFINTEGRABLEHAMILTONIANSYSTEMSGaoPuyun(高普云)(DepartmentofMathematics,NanjingUniversity,Nanijing210?..  相似文献   

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EDITORIALCOMMITTEEOF"APPLIEDMATBEMATICSANDMECHANICS"Editor-in-chief:ChienWeizang(钱伟长)ViceEditor-in-chief:'TanHaosheng(谈镐生),Ye...  相似文献   

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利用形状记忆合金降低结构的应力集中研究   总被引:1,自引:0,他引:1  
王征  熊克 《实验力学》1997,12(1):64-69
形状记忆合金(SMA)由于具有形状记忆效应(SME),可以用于改善承载结构中受损伤部位的应力、应变分布,降低危险区域的应力集中。本文介绍了这项新技术,并以各向同性材料的带孔板的理论分析与实验说明它的可行性  相似文献   

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MIXEDCOMPATIBLEELEMENTANDMIXEDHYBRIDINCOMPATIBLEELEMENTVARIATIONALMETHODSINDYNAMICSOFVISCOUSBAROTROPICFLUIDSShenXiao-ming(沈孝明...  相似文献   

10.
THEMETHODOFDERIVATIONOFMAC-MILLAN'SEQUATIONFORTHENON-LINEARNON-HOLONOMICSYSTEM¥QiuRong(邱荣)(DepartmentofPhysics,FuzhouUniversi...  相似文献   

11.
韩文娟  刘海 《力学与实践》2010,32(4):109-111
对《力学》中的物体自由度进行多方面分析,以深化教学、提高学生正 确分析物理问题的能力.使用实际教学分析的研究方法,在《力学》范围内讨论自由度与坐标、 自由与约束的关系并得以下结论: (1) 同一物体的自由度随其所在的``空间'不同而不同, 不因坐标系的选取不同而 异, 在同类参考系中不因参考系的动静而有别;(2)自由度遵循叠加原理. 讨论了质点系的总自由度及相关计算问题,并指出研究《力学》中自由度的意义.  相似文献   

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The present paper deals with development and design of new methods utilizing Wiedemann's effect for determination of state of strain in building structures. Wiedemann's effect and some features of torsional strain of magnetic field are the basis of new experimental method. Especially the point electromagnetic strain gages using the effect of pure torsion of electromagnetic field to enable universal examination. For strain-gage measurements, almost all physical quantities are used which can be related to the variation in length of the structures. From the electric strain measurements, the most commonly used methods are the measurements by resonance-wire strain gages or by electric-resistance strain gages. In this paper, electromagnetic strain gages are discussed using the Wiedemann effect, and the author describes some new measuring equipment and his own suggestions and methods based on an application of this effect.  相似文献   

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The exact solutions of the nonlinear equations of filtration of an aerated liquid have been obtained in [1–3]. In [4] the system of equations of an aerated liquid have been reduced to the heat-conduction equation under certain assumptions. An approximate method of computing the nonsteady flow of an aerated liquid is given in [5], where the real flow pattern is replaced by a computational scheme of successive change of stationary states. In [6] the same problem is solved by the method of averaging. In the present article estimates of the solution of the equations for nonstationary filtration of an aerated liquid in one-dimensional layer are constructed under certain conditions imposed on the desired functions. These estimates can be used as approximate solutions with known error or for the verification of the accuracy of different approximate methods. We note that the use of comparison theorem for the estimate of solutions of equations of nonlinear filtration is discussed in [7–9]. The methods of constructing estimates of solutions of various problems of heat conduction are given in [10, 11]  相似文献   

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It is well known that the problem on nonseparating potential flow of an incompressible fluid about an array of profiles reduces to an integral equation for a certain real function, determined on the contours of the profiles of the array. As such a function one can take, as was done, for instance, in [1–5], the relative velocity of the fluid on the profiles of the array. For arrays of profiles of arbitrary shape it is necessary to solve the corresponding integral equation numerically. In the particular examples of the calculation of aerodynamic arrays that are available [1–3] the numerical methods used were based on the approximate evaluation of contour integrals by rectangle formulas. As investigations showed, sizeable errors arose thereby in the approximate solution obtained, these being especially significant in the case of curved profiles of relatively small bulk. In the present paper a method for the numerical solution of the integral equation obtained in [5] is proposed. The method is based on the replacement of a profile of the array with an inscribed N polygon, the length of whose sides is of the order N–1 and whose internal angles are close to . Convergence with increasing N of the numerical solution to an exact solution of the integral equations at the reference points is demonstrated. Examples of the calculation are given.Novosibirsk. Translated from Izvestiya Akademii Nauk SSSR. Mekhanika Zhidkosti i Gaza, No. 2, pp. 105–112, March–April, 1972.  相似文献   

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