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Chinese translation for "hamilton principle"

哈密顿原理

Related Translations:
lewis hamilton:  汉弥尔顿刘易斯・咸美顿易斯咸美
hamilton lashley:  汉密尔顿拉什利
jim hamilton:  副总裁汉弥尔顿吉姆汉米尔顿
fort hamilton:  汉弥尔顿堡
linda hamilton:  琳达.汉密尔顿琳达汉弥顿
hamilton standard:  汉密尔顿标准公司
new hamilton:  新哈密尔顿
tom hamilton:  汤姆汉密尔顿
hamilton river:  哈密尔顿河
hamilton zoo:  汉密尔顿动物园
Example Sentences:
1.Generalized hamilton principle
广义哈密顿原理
2.Hamilton principle can be used in holonomic system and intrinsical linear nonholnomic system . the formulas of them are unified . hamiltonian action is stability in intrinsical linear nonholnomic system
本文将hamilton原理应用到本质线性非完整系统,首次证明了在本质线性非完整系统中, hamilton作用量为稳定的作用量;将完整系统和本质线性非完整系统的hamilton原理从形式和本质上统一起来。
3.First , the dynamic stability of braid composite cylindrical shells with the influences of some main factors is introduced . the general governing equations for the nonlinear dynamic stability is obtained . by the hamilton principle . the creep buckling analysis of braid composite cylindrical shells under axial compression and the dynamic stability under nonconservation force are discussed as emphases . in creep buckling question , by means of theoretical analysis , the instaneous critical load and durable critical load of viscoelastic braid composite cylindrical shell under axial compression are obtained and the numerical example is given
首先介绍了编织复合材料圆柱壳在几种主要因素影响下的动力稳定性问题,用hamilton原理建立非线性动力稳定性问题的一般性基本方程。然后重点讨论了编织复合材料圆柱壳轴压下的蠕变屈曲问题及非保守力作用下的屈曲问题。对蠕变屈曲问题,通过理论分析来得到了编织复合材料圆柱壳的瞬时弹性临界载荷和持久临界载荷,给出了具体的算例。
4.They are studied that the nonlinear problem and un - determinate problem of virtual displacement in nonholonomic system in the second chapter . in chapter 3 , they are studied that chetaev model and vacco model in nonholonomic system . a unified form of hamilton principle in intrinsical linear nonholonomic system is studied in chapter 4
第一章对非完整动力学研究的有关现状进行了综合评述;第二章研究了非完整系统虚位移关系的不定性问题与非线性问题;第三章比较研究了一般非完整系统的chetaev模型和vacco模型;第四章研究了本质线性非完整系统的hamilton原理;第五章给出了本文的结论与有关研究的展望。
5.In the beginning of this thesis , types and characteristics of intelligent material elements have been introduced . and the basic equations of piezoelectric material have been given . then according to hamilton principle , both the static and dynamic finite element equations for the intelligent structure are formulated with isoparametric element of bending plate or bending beam
在本论文的开始,简要介绍了智能材料元件的种类和性质,并给出了压电材料的本构方程,然后根据hamilton原理,采用任意等参四边形板梁弯曲单元,导出了智能梁的静态、动态有限元方程;对于复杂几何形状或边界条件的一般结构,根据三维有限元模型,导出三维动态有限元方程。
6.To study the influence of this damper configuration to aeromechanical stability , some work has been done in this thesis . first , dynamic equation of the rotor - hub system was modeled with the generalized hamilton principle , which can be used to analyze the stability problem in different conditions like on - ground , hovering and flight . when fastening the fuselage , the model can also be used to analyze the stability problem of isolated rotor system
为了研究这种新型布置减摆器对直升机稳定性的影响,本文所作研究工作如下:首先,本文利用广义的hamilton原理建立了适用于不同状态(地面、悬停和前飞)的旋翼/机体耦合系统的动力学模型,该模型中将机体固定可以用来分析孤立旋翼的稳定性问题。
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