Inequalities relating to L_p-version of Petty's conjectured projection inequality

Petty's conjectured projection inequality is a famous open problem in the theory of convex bodies.In this paper,it is shown that an inequality relating to L_p-version of the Petty's conjectured projection inequality is developed by using the notions of the L_p-mixed volume and the L_p-dual mixed volume,the relation of the L_p-projection body and the geometric bodyΓ_(-p)K,the Bourgain-Milman inequality and the L_p-Busemann- Petty inequality.In addition,for each origin-symmetric convex body,by applying the Jeusen inequality and the monotonicity of the geometric bodyΓ_(-p)K,the reverses of L_p-version of the Perry's conjectured projection inequality and the L_p-Petty projection inequality are given,respectively.     

航行器部件流体动力外形仿生初探

本文简要地介绍了航行器的两种部件流体动力外形仿生的构造特点和模型实验方法，同时给出了主要的实验结果，其中仿鲨鱼头的细长椭锥在大迎角时的侧力减小为圆锥的２３％，采用波纹壁面相对厚度为１３％的机翼的摩阻比光洁翼面的减少了９％。     

Stress concentration of an ellipsoidal inclusion of revolution in a semi-infinite body under biaxial tension

Summary This paper deals with the stress concentration problem of an ellipsoidal inclusion of revolution in a semi-infinite body under biaxial tension. The problem is formulated as a system of singular integral equations with Cauchy-type or logarithmic-type singularities, where unknowns are densities of body forces distributed in the r- and z-directions in semi-infinite bodies having the same elastic constants as the ones of the matrix and inclusion. In order to satisfy the boundary conditions along the ellipsoidal boundary, four fundamental density functions proposed in [24, 25] are used. The body-force densities are approximated by a linear combination of fundamental density functions and polynomials. The present method is found to yield rapidly converging numerical results for stress distribution along the boundaries even when the inclusion is very close to the free boundary. The effect of the free surface on the stress concentration factor is discussed with varying the distance from the surface, the shape ratio and the elastic modulus ratio. The present results are compared with the ones of an ellipsoidal cavity in a semi-infinite body.accepted for publication 11 November 2003     

自旋液体晃动Pfeiffer方法的分析

本文对研究自旋液体晃动的Pfeiffer方法提出了一种分析方法,从而将液体自由振动的稳定性的Pfeiffer方法推广于既有重力又有自旋的液体晃动的研究。     

参数激励的刚体混沌运动

讨论定点运动或圆轨道上运动的自由刚体，由于其内部或外部附件转动或振动引起转动惯量的周期变化，使系统受到周期的激励，而成为一受周期扰动的近Ｅｕｌｅｒ情形的运动刚体。通过计算动力学方程宿轨道的Ｍｅｌｎｉｋｏｖ函数，以及Ｐｏｉｎｃａｒｅ截面的数值计算，证明系统具有Ｓｍａｌｅ马蹄意义下的混沌。     

Dynamic analysis of a disc brake under frictional and thermomechanical internal loading

The study of the vibratory response of a mechanical system as complex as a disc brake needs to consider the complexity of the problem induced by the coupling of tribological, thermomechanical and dynamical effects. Experimental consideration are discussed here for two set ups at the full scale of the disc brake and at a local scale focussed on the third body interface. A numerical model with thermomechanical and dynamical couplings is then presented, followed by a substantial discussion.     

矩形压电体中反平面裂纹的电弹性场

基于线性压电理论,本文获得了含有中心反平面裂纹的矩形压电体中的奇异应力和电场。利用Fourier积分变换和Fourier正弦级数将电绝缘型裂纹问题化为对偶积分方程,并进一步归结为易于求解的第二类Fred-holm积分方程。获得了裂纹尖端应力、应变、电位移和电场的解析解,求得了裂纹尖端场的强度因子及能量释放率。分析了压电矩形体的几何尺寸对它们的影响。结果表明,对于电绝缘型裂纹,裂纹尖端附近的各个场变量都具有-1/2阶的奇异性,能量释放率与电荷载的方向及大小有关,并且有可能为负值。     

面向载体自转的无陀螺捷联惯导系统

鉴于大多数无陀螺捷联惯导系统忽略载体质心位置和加速度计组件中心位置之间的距离，从理论上推导出了面向载体自转的无陀螺捷联惯导系统的基本方程，分析了载体自转对无陀螺捷联惯导系统性能的影响，为无陀螺捷联惯导系统进一步提高导航精度奠定基础。     

DYNAMIC ANALYSIS OF FLEXIBLE BODY WITH DEFINITE MOVING ATTITUTE

The nonlinear dynamic control equation of a flexible multi-body system with definite moving attitude is discussed.The motion of the aircraft in space is regarded as known and the influence of the flexible structural members in the aircraft on the motion and attitude of the aircraft is analyzed.By means of a hypothetical mode,the defor- mation of flexible members is regarded as composed of the line element vibration in the axial direction of rectangular coordinates in space.According to Kane’s method in dy- namics,a dynamic equation is established,which contains the structural stiffness matrix that represents the elastic deformation and the geometric stiffness matrix that represents the nonlinear deformation of the deformed body.Through simplification the dynamic equation of the influence of the planar flexible body with a windsurfboard structure on the spacecraft motion is obtained.The numerical solution for this kind of equation can be realized by a computer.