各向同性材料的英文

• isotrocpic material
• isotropic materials

• "各向同性"英文翻译    isotropy
• "材料"英文翻译    material
• "横向同性材料" 英文翻译 :    transversely isotropic material
• "各向同性层压材料" 英文翻译 :    isotropic laminate
• "各向同性的材料" 英文翻译 :    isotropic material
• "各向同性记忆材料" 英文翻译 :    isotropic material with memory
• "各向同性透明材料" 英文翻译 :    isotropic transparent material
• "各向同性" 英文翻译 :    [物理学] isotropy
• "各向同性板" 英文翻译 :    isotropic plate; isotropic-piston
• "各向同性的" 英文翻译 :    isotropic; isotropous; isotropy
• "各向同性点" 英文翻译 :    isotropic point
• "各向同性化" 英文翻译 :    isotropization
• "各向同性体" 英文翻译 :    isotrope; isotropic body
• "各向同性源" 英文翻译 :    isotropic source
• "均质；各向同性" 英文翻译 :    isotrope
• "类各向同性" 英文翻译 :    quasi isotropy
• "伪各向同性" 英文翻译 :    quasi isotropy; quasiisotropy
• "准各向同性" 英文翻译 :    quasi-isotropic
• "高密度各向同性炭材料" 英文翻译 :    hdic
• "弹性各向同性" 英文翻译 :    elastic anisotropy; elastic isotropy; elastically isotropic
• "非各向同性的" 英文翻译 :    non isotropic; non-isotropic
• "各向同性层压" 英文翻译 :    isotropic lamination
• "各向同性弹性" 英文翻译 :    isotropic elasticity
• "各向同性点源" 英文翻译 :    isotopic point source; isotropic point source
• "各向同性对称" 英文翻译 :    isotropic symmetry

• For the sake of simplicity only a material with isotropic properties will be considered .
  为了简单起见，仅讨论各向同性材料。
• A stress - strain relation of an isotropic material to be in elastic anisotropic damage
  各向同性材料受各向异性弹性损伤时的应力应变关系
• With the stress ( strain ) and coupling coefficient being ignored , the coupling heat conduction equation and the coupling moisture diffusion equation would degenerate to fourier heat conduction model and pick diffusion model respectively
  并针对各向同性材料，导出含湿、热的耦合线性粘弹性本构方程，以及相应的热传导方程和耦合湿分扩散方程。
• In the first part of this thesis , history of ptr technology and measuring equipment were introduced . we have summarized the continuously modulating ptr theory of isotropic materials , and formed a complete system info concluding one dimension and three dimensions theories , monolayer and multilayer theories
  本文前半部分简单叙述了ptr技术的研究历史和测量装置，较为系统地总结了各向同性材料的连续调制ptr理论，形成了从一维到三维、从单层至侈层的完整理论体系。
• The main work lists as following : 1 on the condition that cfrc is an macroscopically isotropic material , the governing equations of electric and thermal conduction for the inspection were established ; the current density and joule heat distribution around several kinds of flaws were investigated 2 by fem , the process of inspection was simulated ; the current density , joule heat and temperature distribution were also investigated , and the simulation results were contrasted with experimental data
  主要工作为： 1 、将机敏混凝土合理假定为宏观各向同性材料的基础上，建立了检测过程中的热、电传导相关的控制方程；并研究了几种不同缺陷周围检测过程中的电流密度、焦耳热分布规律。 2 、通过有限元方法对机敏混凝土的电热场进行了模拟分析，研究电流密度、焦耳热分布及试件表面温度分布变化规律并与实验所得试件表面温度场进行了对比分析研究。
• ( 1 ) assuming that the gfrp rods is transversely isotropic material . derive the micro - mechanical model of splitting failure in concrete reinforced with gfrp rods . analysis the stress and its distribution of the cracked concrete around the gfrp rods , finding the relations of the number of cracks and the crack radius and the stress around the interface of concrete and gfrp rods
  ( 1 )将玻璃钢筋视为横观各向同性材料，推导了gfrp筋增强混凝土劈裂失效的细观力学模型，分析了玻璃钢筋周围混凝土开裂时的应力及其分布情况，得到了裂纹数量、开裂半径与玻璃钢筋/混凝土界面周围应力的定量关系。
• We have divided the constitutive relation equation into the distortion equation and the dilatation equation and extended elasticity recovery correspondence principle that has one independence material function to the conditions of two independence material functions , a three dimensional nonlinear viscoelastic constitutive relations are also given
  我们将本构方程分解为畸变方程和体变方程，把弹性回复对应原理由两个材料函数成比例推广到两个独立的材料函数的情况，同时给出了三维各向同性材料的非线性粘弹性本构关系。
• Because the propellant grain is viscoelastic material , the liner and adiabatic layer are also viscoelastic one , the interface debond problem is actually interface crack about elastic - viscoelastic or bi - viscoelastic materials . research about this problem relates to the knowledge of viscoelastic mechanics and interface fracture and combustion . numerical analysis method about interface debond on solid rocket motor is researched in this paper
  由于固体火箭发动机的推进剂药柱是一种粘弹性材料,衬层和绝热层也具有粘弹性性质,因此其界面脱粘问题实际上是弹性-粘弹性或双粘弹性各向同性材料界面裂纹问题,对该问题的研究涉及到粘弹性力学、界面断裂力学和燃烧学等相关学科。

• 各向同性材料的日语：とうほうせいざいりょう