限分析的英文

• limit analysis

• "分析"英文翻译    analyse
• "极限分析" 英文翻译 :    limit analysis; ultimate analysis
• "极限分析法" 英文翻译 :    limit analysis method
• "容限分析" 英文翻译 :    tolerance analysis
• "规范分析；界限分析" 英文翻译 :    threshold analysis
• "额定运行极限分析" 英文翻译 :    test of rated service limiting breaking capacity
• "极限分析补强法" 英文翻译 :    limit analysis method of reinforcement; limitanalysismethodofreinforcement
• "限分" 英文翻译 :    limited e.g. limited culpability by reason of accident unintentional error
• "分析土坡稳定极限分析法" 英文翻译 :    limit analysis method of slope stability
• "购货欠款赊欠期限分析表" 英文翻译 :    purchase liabilities agint schedule
• "土坡稳定极限分析法" 英文翻译 :    limit analysis method of slope stability
• "信息流程时限分析法" 英文翻译 :    information through and timing
• "土坡稳定分析土坡稳定极限分析法" 英文翻译 :    limit analysis method of slope stability
• "油田稳产界限分析方法研究" 英文翻译 :    an analysis method of stable production limits for oil fields
• "超限分" 英文翻译 :    excess points
• "超限分辨" 英文翻译 :    superresolution
• "带限分辨率" 英文翻译 :    bandlimited resolution
• "负二限分布" 英文翻译 :    negative binomial distribution
• "极限分辨角" 英文翻译 :    limiting angle of resolution; limiting resolution angle
• "极限分辨力" 英文翻译 :    limiting resolution; ultimate resolution
• "极限分辨率" 英文翻译 :    limit resolution; limiting resolution; limiting resolving power; limitingresolution
• "极限分辩率" 英文翻译 :    limiting resolution
• "极限分布" 英文翻译 :    limit distribution; limiting distribution
• "极限分解力" 英文翻译 :    limiting resolution; limiting vertical resolution
• "极限分离" 英文翻译 :    ultimate separation

• B ased on the analysis o f performance limit of turbo codes , it is made clear that the distance spectrum in optimizing codes is the objective of designing optimal interleaver
  在对turbo码性能限分析的基础上，指出优化码字的距离谱是优化交织器设计的准则，并提出了扩散度的概念。
• Then an integrated application program including some functional modules such as residual strength analysis , crack growth analysis , principle structure elements database management , material properties database management etc , with friendly interfaces and favorable windows styles , is developed by using these classes . finally all of the typical structures described in the " damage tolerance design handbook " have been analyzed
  在此基础上研制了具有友好界面和良好windows风格的损伤容限分析与评定应用程序，并完成了《设计手册》中给定的全部典型开裂结构的实例化，实现了对这些结构的裂纹扩展分析和剩余强度分析。
• The work of this thesis has shown that the object - oriented damage tolerance program does require much less time and is indeed more suitable than procedure - oriented programming in damage tolerance analysis of engineering structures . furthermore , the damage tolerance analysis classes have excellent ability in hierarchy and extension , so they are great valuable in engineering and will be used more widely in the future
  本文工作表明，采用面向对象技术所建立的损伤容限分析类库具有良好的继承性和可扩充性，不仅可以使软件性能和适用性得到显著提高，而且还可以大大缩短软件开发周期，在工程上具有良好的应用价值和应用前景。
• For the fine solution of this problem , the author has made an attempt to introduce the object - oriented technique to damage tolerance analysis . a set of basic and auxiliary classes , based upon some important concepts of object - oriented technique , which can be directly used for the development of programs of damage tolerance analysis has been designed and implemented by c + + language
  为此，本文将面向对象的程序设计方法引入到损伤容限分析中，运用面向对象观点对损伤容限分析方法和数据需求作了全面分析，设计了一套损伤容限分析的基本类库和辅助类库，建立了损伤容限分析的对象模型，并采用c + +语言进行了实现。
• As the damage tolerance technique has being widely and deeply adopted in the design and life prediction of aircraft structures , the development of high performance and more suitable software used in damage tolerance design and assessment is more urgent . while at the same time the existing domestic software is not well suitable for requirements in engineering
  随着损伤容限技术在飞机结构设计和寿命评估中的广泛采用，研制高性能且实用的损伤容限分析与评定软件系统越来越迫切，而国内现有的损伤容限分析软件经实践证明其性能和适用性不能很好满足工程需要，特别是结构剩余强度和裂纹扩展分析程序。
• The second part concerns about the fracture analysis of cracked metalic structures . the last part investigates the behavior of impact dents on aircraft windshield glass and their possibility to be analyzed using fracture mechanics . in chapter 1 , a review is made to the resent developments of cumulative damage models and fatigue life prediction methodology of composite laminates
  本论文研究飞机结构疲劳和损伤容限分析中的若干问题，按研究的对象(材料、结构)可以大致划分为三个组成部分：复合材料层压结构疲劳分析，第一章第三章；金属结构断裂分析，第四、五章；座舱盖玻璃撞击损伤的断裂分析，第六章。