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为便于力学科研人员及时了解2010年度基金项目申请信息,现将数理科学部力学科学处受理的面上项目、青年基金项目、地区基金项目、重点项目、国家杰出青年科学基金和海外及港澳学者合作研究基金项目的申请情况做一介绍. 相似文献
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为便于力学专家及时了解2000年度力学学科的基金项目申请,现将面上项目、重点项目、国家杰出青年科学基金及海外(香港)青年学者合作研究基金项目的受理情况做一介绍.1面上项目 2000年力学学科面上各类项目的申请数及与去年的对比见表1. 今年面上项目申请总数比去年减少37项.其中,自由申请项目和青年基金项目各减少24项和 19项,地区基金项目和高技术探索项目分别增加 2项和 4项. 力学学科各分支学科的申请项目见表2. 其中一般力学的申请项数占总申请项数的13.7%,固体力学占48.0%,流体力学占27.… 相似文献
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为便于力学专家及时了解2004年度基金项目申请信息,将数理科学部力学科学处受理的面上项目、重点项目、国家杰出青年科学基金、海外及中国香港、澳门特别行政区青年学者合作研究基金项目的申请情况做一介绍. 相似文献
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为便于力学专家及时了解2002年度力学学科的基金项目申请,将面上项目、重点项目、国家杰出青年科学基金及海外(香港、澳门)青年学者合作研究基金项目的受理情况做一介绍. 相似文献
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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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Tibor Javor 《Experimental Mechanics》1968,8(4):171-176
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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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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