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切削颤振方程探讨
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作者 樊社新 《广西大学学报(自然科学版)》 CAS CSCD 2002年第3期222-224,共3页
对传统切削颤振理论用共振法决定等效参数进行了讨论 。
关键词 切削颤振方程 等效参数 切削颤振理论 机械加工 共振法 颤振机理
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全弹颤振运动方程
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作者 崔广 《战术导弹技术》 1988年第4期12-22,共11页
本文推导了全弹颤振运动方程。它适用于具有竖直对称平面的弹体;弹身上可以有任意组升力面;每组升力面可以是“-”形、“+”形、倒“T”形、倒“Y”形、“V”形、倒“V”形和“X”形(包括上、下反角均为45°的“X”形,上、下反角不... 本文推导了全弹颤振运动方程。它适用于具有竖直对称平面的弹体;弹身上可以有任意组升力面;每组升力面可以是“-”形、“+”形、倒“T”形、倒“Y”形、“V”形、倒“V”形和“X”形(包括上、下反角均为45°的“X”形,上、下反角不等的“X”形和上、下翼面不同的“X”形)等形状,每片升力面有任意个弹性变形自由度。扼要讨论了气动压力计算问题。 展开更多
关键词 颤振分析(0601) 导弹弹体 颤振——运动方程 气动力计算——分析
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资金项目:国家自然科学基金资助项目
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作者 牟让科 杨永年 《应用力学学报》 CAS CSCD 北大核心 2001年第z1期185-188,共4页
采用能计及非线性结构刚度的颤振方程为控制方程,和非定常N-S方程耦合求解,运用龙格-库塔方法在时域内求解结构响应的时间历程,从而确定颤振临界条件.计算了带结构刚度非线性的跨音速颤振特性.计算结果表明,结构刚度非线性对颤振特性有... 采用能计及非线性结构刚度的颤振方程为控制方程,和非定常N-S方程耦合求解,运用龙格-库塔方法在时域内求解结构响应的时间历程,从而确定颤振临界条件.计算了带结构刚度非线性的跨音速颤振特性.计算结果表明,结构刚度非线性对颤振特性有明显的影响.由于同时具有结构和气动力非线性,导致了具有复杂振荡极限环的特性. 展开更多
关键词 跨音速颤振 结构刚度非线性 N-S方程
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一般复矩阵特征根和特征矢量求解及运用
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作者 王磊 董文俊 《机械设计与研究》 CSCD 北大核心 2010年第4期12-14,共3页
颤振方程在频率内的求解方法是通过状态方程中实矩阵的特征根和特征矢量求解来完成的。通过直接求解颤振方程中的复矩阵来计算颤振频率和颤振速度的,同时详细推导了一般复矩阵的特征根和特征矢量的计算过程。最后利用复矩阵求解特征根... 颤振方程在频率内的求解方法是通过状态方程中实矩阵的特征根和特征矢量求解来完成的。通过直接求解颤振方程中的复矩阵来计算颤振频率和颤振速度的,同时详细推导了一般复矩阵的特征根和特征矢量的计算过程。最后利用复矩阵求解特征根和特征矢量的原理,用P-K法解决了颤振方程中颤振问题。 展开更多
关键词 颤振方程 复矩阵 特征根:特征矢量 特征根追寻技术
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Flutter analyses of complete aircraft based on hybrid grids and parallel computing 被引量:6
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作者 ZHENG GuanNan YANG GuoWei QIAN Wei 《Science China(Technological Sciences)》 SCIE EI CAS 2013年第2期398-404,共7页
A tightly coupled method was developed to analyse aeroelasticity by constructing subiterative schemes for fluid and structural equations of motion,respectively.With MPI partition parallel computing,the fluid was solve... A tightly coupled method was developed to analyse aeroelasticity by constructing subiterative schemes for fluid and structural equations of motion,respectively.With MPI partition parallel computing,the fluid was solved by Navier-Stokes equations based on hybrid grids.A new unstructured background grid deformtion method was used for the CFD grid deformation.The transonic flutter wind tunnel model of a complete aircraft was simulated to validate the developed method.The flutter characteristics of the aircraft was analysed and compared with the test results.It indicates that the devoloped method has a relatively higher precision and can be used for aeronautical engineering application. 展开更多
关键词 CFD CSD aeroelasticity coupled method FLUTTER MPI
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Milling stability analysis using the spectral method 被引量:11
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作者 DING Ye ZHU LiMin +1 位作者 ZHANG XiaoJian DING Han 《Science China(Technological Sciences)》 SCIE EI CAS 2011年第12期3130-3136,共7页
This paper focuses on the development of an efficient semi-analytical solution of chatter stability in milling based on the spectral method for integral equations. The time-periodic dynamics of the milling process tak... This paper focuses on the development of an efficient semi-analytical solution of chatter stability in milling based on the spectral method for integral equations. The time-periodic dynamics of the milling process taking the regenerative effect into account is formulated as a delayed differential equation with time-periodic coefficients, and then reformulated as a form of integral equation. On the basis of one tooth period being divided into a series of subintervals, the barycentric Lagrange interpolation polynomials are employed to approximate the state term and the delay term in the integral equation, respectively, while the Gaussian quadrature method is utilized to approximate the integral tenn. Thereafter, the Floquet transition matrix within the tooth period is constructed to predict the chatter stability according to Floquet theory. Experimental-validated one-degree-of-freedom and two-degree-of-freedom milling examples are used to verify the proposed algorithm, and compared with existing algorithms, it has the advantages of high rate of convergence and high computational efficiency. 展开更多
关键词 milling stability delayed differential equation integral equation spectral method Floquet theory
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