期刊文献+
共找到7篇文章
< 1 >
每页显示 20 50 100
螺栓球节点对钢管杆件屈曲特征值的影响
1
作者 吴志豪 张辰啸 +2 位作者 贾冬云 王鸿宇 傅阳 《安徽工业大学学报(自然科学版)》 CAS 2024年第1期74-80,共7页
利用ANSYS软件建立螺栓球节点与钢管杆组合构件的有限元模型,采用接触模拟法计算螺栓球钢管构件的屈曲特征值,分析螺栓球节点作为杆件两端约束时对杆件临界荷载产生的影响;参数化研究螺栓半径、套筒壁厚、封板厚度、螺栓头半径和套筒长... 利用ANSYS软件建立螺栓球节点与钢管杆组合构件的有限元模型,采用接触模拟法计算螺栓球钢管构件的屈曲特征值,分析螺栓球节点作为杆件两端约束时对杆件临界荷载产生的影响;参数化研究螺栓半径、套筒壁厚、封板厚度、螺栓头半径和套筒长度等因素对不同长细比杆件屈曲特征值的影响;基于杆件屈曲的欧拉公式,通过回归分析获得考虑螺栓球节点参数与杆件长细比影响杆件的屈曲特征值计算公式。结果表明:随螺栓半径和套筒壁厚增大杆件屈曲特征值显著增大,螺栓头半径对其的影响可忽略不计,封板厚度的增加和套筒长度的减小也能使杆件屈曲特征值有所增加;随杆件长细比的增大,以上各因素对杆件屈曲特征值的影响均逐渐减小,同时杆件长细比越大螺栓球节点对杆件的约束越强;利用回归分析获得组合构件屈曲特征值公式的计算值与有限元结果接近,随节点参数与杆件长细比的变化趋势一致,该公式能够较精准地计算杆件屈曲特征值。 展开更多
关键词 接触模拟法 螺栓球节点 杆件 欧拉公式 参数化 屈曲特征值
下载PDF
Numerical algorithm for rigid body position estimation using the quaternion approach 被引量:2
2
作者 Miodrag Zigic Nenad Grahovac 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2018年第2期400-408,共9页
This paper deals with rigid body attitude estimation on the basis of the data obtained from an inertial measurement unit mounted on the body. The aim of this work is to present the numerical algorithm, which can be ea... This paper deals with rigid body attitude estimation on the basis of the data obtained from an inertial measurement unit mounted on the body. The aim of this work is to present the numerical algorithm, which can be easily applied to the wide class of problems concerning rigid body positioning, arising in aerospace and marine engineering, or in increasingly popular robotic systems and unmanned aerial vehicles. Following the considerations of kinematics of rigid bodies, the relations between accelerations of different points of the body are given. A rotation matrix is formed using the quaternion approach to avoid singularities. We present numerical procedures for determination of the absolute accelerations of the center of mass and of an arbitrary point of the body expressed in the inertial reference frame, as well as its attitude. An application of the algorithm to the example of a heavy symmetrical gyroscope is presented, where input data for the numerical procedure are obtained from the solution of differential equations of motion, instead of using sensor measurements. 展开更多
关键词 Rigid body KINEMATICS Inertial measurement unit euler parameters QUATERNION
下载PDF
Compression of the North Hemisphere derived from space geodesy 被引量:1
3
作者 金双根 朱文耀 《Acta Seismologica Sinica(English Edition)》 CSCD 2003年第1期99-106,共8页
The convergent and divergent velocities of active plate boundaries in the North Hemisphere are obtained with space geodetic data. The relative motions of adjacent plates in north-south direction are almost convergent;... The convergent and divergent velocities of active plate boundaries in the North Hemisphere are obtained with space geodetic data. The relative motions of adjacent plates in north-south direction are almost convergent; the spreading rates of the north mid-Atlantic ridge are smaller than the south mid-Atlantic ridge; the closed differences of the baseline length rates between stations on different plates along the latitudinal circle of 7.7, 23.3? 34.8? 42.0?and 51.0?are all negative. All these show that the North Hemisphere is a compressive hemisphere. 展开更多
关键词 space geodesy North Hemisphere compression euler parameter
下载PDF
Quaternion methods and models of regular celestial mechanics and astrodynamics
4
作者 Y.N.CHELNOKOV 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI CSCD 2022年第1期21-80,共60页
This paper is a review,which focuses on our work,while including an analysis of many works of other researchers in the field of quaternionic regularization.The regular quaternion models of celestial mechanics and astr... This paper is a review,which focuses on our work,while including an analysis of many works of other researchers in the field of quaternionic regularization.The regular quaternion models of celestial mechanics and astrodynamics in the Kustaanheimo-Stiefel(KS)variables and Euler(Rodrigues-Hamilton)parameters are analyzed.These models are derived by the quaternion methods of mechanics and are based on the differential equations of the perturbed spatial two-body problem and the perturbed spatial central motion of a point particle.This paper also covers some applications of these models.Stiefel and Scheifele are known to have doubted that quaternions and quaternion matrices can be used efficiently to regularize the equations of celestial mechanics.However,the author of this paper and other researchers refuted this point of view and showed that the quaternion approach actually leads to efficient solutions for regularizing the equations of celestial mechanics and astrodynamics.This paper presents convenient geometric and kinematic interpretations of the KS transformation and the KS bilinear relation proposed by the present author.More general(compared with the KS equations)quaternion regular equations of the perturbed spatial two-body problem in the KS variables are presented.These equations are derived with the assumption that the KS bilinear relation was not satisfied.The main stages of the quaternion theory of regularizing the vector differential equation of the perturbed central motion of a point particle are presented,together with regular equations in the KS variables and Euler parameters,derived by the aforementioned theory.We also present the derivation of regular quaternion equations of the perturbed spatial two-body problem in the Levi-Civita variables and the Euler parameters,developed by the ideal rectangular Hansen coordinates and the orientation quaternion of the ideal coordinate frame.This paper also gives new results using quaternionic methods in the perturbed spatial restricted three-body problem. 展开更多
关键词 celestial mechanics ASTRODYNAMICS perturbed spatial two-body problem central motion REGULARIZATION Levi-Civita and Kustaanheimo-Stiefel(KS)variables euler parameter QUATERNION
下载PDF
运输类飞机翼身组合体参数化及快速气动力计算研究 被引量:1
5
作者 左志成 段卓毅 陈迎春 《空气动力学学报》 EI CSCD 北大核心 2006年第2期246-249,共4页
飞机方案设计阶段,迫切需要一个能够快速评估、计算不同参数组合的翼身组合体基本气动力特性的分析平台。为满足这一实际工程设计需要,本文提出运输类飞机参数化概念和具体研究方法,结合运输机气动布局设计的基本准则,应用计算机图形学... 飞机方案设计阶段,迫切需要一个能够快速评估、计算不同参数组合的翼身组合体基本气动力特性的分析平台。为满足这一实际工程设计需要,本文提出运输类飞机参数化概念和具体研究方法,结合运输机气动布局设计的基本准则,应用计算机图形学进行辅助设计,利用丰富的参数曲线,如NURBS曲线、贝塞尔曲线、拉格朗日插值等方法描述复杂的翼身组合体外形,开发了快速分析计算翼身组合体气动力特性分析平台,实现了从总体方案初步设计到MGAERO软件数值模拟的无缝过渡,并结合具体算例验证了方法的可行性和工程实用价值。 展开更多
关键词 数值计算 参数化 气动计算模型 欧拉方程 附面层修正
下载PDF
民机翼身组合体参数化研究 被引量:2
6
作者 左志成 段卓毅 陈迎春 《飞机设计》 2005年第2期20-25,共6页
飞机方案设计阶段,迫切需要一个能够快速评估、计算不同参数组合的翼身组合体基本气动力特性的分析平台。为满足这一实际工程设计需要,本文提出运输类飞机参数化概念和具体研究方法,开发了快速分析计算翼身组合体气动力特性分析平台,结... 飞机方案设计阶段,迫切需要一个能够快速评估、计算不同参数组合的翼身组合体基本气动力特性的分析平台。为满足这一实际工程设计需要,本文提出运输类飞机参数化概念和具体研究方法,开发了快速分析计算翼身组合体气动力特性分析平台,结合具体算例验证了方法的可行性和工程实用价值。 展开更多
关键词 民用客机 翼身组合体 参数化 数值计算 欧拉方程
下载PDF
A quasi-dynamic model and a symplectic algorithm of super slender Kirchhoff rod 被引量:1
7
作者 Dandan Yang Jianfei Huang Weijia Zhao 《International Journal of Modeling, Simulation, and Scientific Computing》 EI 2017年第3期285-295,共11页
Recently the Kirchhoff rod and the methods of dynamical analogue have been widely used in modeling DNA.The features of a DNA such as its super slender and super large deformation raise new challenges in modeling and n... Recently the Kirchhoff rod and the methods of dynamical analogue have been widely used in modeling DNA.The features of a DNA such as its super slender and super large deformation raise new challenges in modeling and numerical simulations of a Kirchhoff rod.In this paper,Euler parameters are introduced to set up the quasi-Hamilton system of an elastic rod,then a symplectic algorithm is applied in its numerical simulations.Finally,a simplified surface model of the rod is given based on the hypothesis of rigid cross-section. 展开更多
关键词 Kirchhoff rod euler parameters quasi-hamilton system symplectic algorithm surface equation
原文传递
上一页 1 下一页 到第
使用帮助 返回顶部