助手标题  
全文文献 工具书 数字 学术定义 翻译助手 学术趋势 更多
查询帮助
意见反馈
   热— 的翻译结果: 查询用时:0.046秒
图标索引 在分类学科中查询
所有学科
更多类别查询

图标索引 历史查询
 

相关语句
  “热—”译为未确定词的双语例句
     In anhydrous solvents: [Sc(SSCN(C_2H_5)2)_3] and (C_2H_5)_2 N~+H_2[Y(SSCN(C_2 H_5)_2)_4] were prcpared, and caractcrized by elemental analy ses, IR and UV spectra, molar conductances, thermogravimetric and differential thermal analyses, and the solubility in some general solvents.
     在无水溶剂中合成了[Sc(SSCN(C_2H_5)_2)_3]及(C_2H_5)_2NH_2·[Y(SSCN(C_2H_5)_2)_4]~-,并通过元素分析、红外光谱、紫外光谱、差热——热重分析和摩尔电导等研究了配合物的性质。
短句来源
     A STUDY ON THERMAL BEHAVIOUR AND THERMAL DECOMPOSITION KINETICS OF UO_2[Bu_2NCO(CH_2)_6CONBu_2](NO_3)_2 BY MEANS OF TG/DTG AND DTA/GC COUPLED SIMULTANEOUS TECHNIQUE ON LINE
     热重法及差热—色谱在线联用技术研究配合物UO_2[Bu_2NCO(CH_2)_6CONBu_2](NO_3)_2的热行为及热分解反应动力学
短句来源
     DTA-GC Combination for Measuring Heat of Adsorption Ⅱ、The Investigation of Differential Heats of Adsorption for Pyridine on γ-Al_2O_3 and Na× Zeolite
     差热-色谱联用法测吸附热——Ⅱ、吡啶在~γ-Al_2O_3及Na×沸石上吸附热的研究
短句来源
     Using this calorimeter, the heat of combustion-AE_C~0 of p-Chlorobenzoic acid was determined to be 3071.49±11.32 kJ/mol.
     并用该仪器测定了对氯苯甲酸的燃烧热—△E~O_t=3071.49±11.32kJ/mol。
短句来源
     DTA-GC Combination for Measuring Adsorption Heat——The Investigation of Differential Heat of Adsorption for Pyridine on γ-Al_2O_3 and NaX Zeolites
     差热-色谱联用法测吸附热——吡啶在γ-Al_2O_3及NaX沸石上吸附热研究
短句来源
更多       
  相似匹配句对
     HOT
     报!
短句来源
     Hotest Word
    
短句来源
     Thermotropic Liquid Crystal——Aromatic Polyesters
     致液晶聚芳酯
短句来源
查询“热—”译词为用户自定义的双语例句

    我想查看译文中含有:的双语例句
例句
为了更好的帮助您理解掌握查询词或其译词在地道英语中的实际用法,我们为您准备了出自英文原文的大量英语例句,供您参考。
  thermo-
The thermo-oxidative degradation of the films is studied by thermogravimetric analysis (TGA).
      
Synthesis and characterization of thermo-sensitive poly (N-isopropylacrylamide) hydrogel with fast response rate
      
Thermo-sensitive poly (N-isopropylacrylamide) (PNIPA) hydrogel with fast response rate was prepared by polymerizing N-isopropylacrylamide (NIPA) in an aqueous hydroxyl-propyl-methyl cellulose solution.
      
The precursor was studied by thermo-gravimetric and differential scanning calorimetry (TG-DSC).
      
The thermal decomposition of CeO2 nanocrystalline precursor prepared by chemical precipitation method was investigated using thermo-gravimetric/differential scanning calorimetry (TG/DSC) and X-ray powder diffraction (XRD).
      
更多          


Wang's theory for determining the approximate configurational partition function of the adsorbed layer is modified in two different ways. One is to assume that the configurational energy should be corrected: the other to advocate that the deficiency due to a wrong expression for the a priori probability of the. central site is more significant.The configurational partition function is evaluated is both methods and the adsorptipn isotherin and the beat of adsorption computed for the case of quadratic lattice...

Wang's theory for determining the approximate configurational partition function of the adsorbed layer is modified in two different ways. One is to assume that the configurational energy should be corrected: the other to advocate that the deficiency due to a wrong expression for the a priori probability of the. central site is more significant.The configurational partition function is evaluated is both methods and the adsorptipn isotherin and the beat of adsorption computed for the case of quadratic lattice With dipole interaction. values for the last two quantities when a uniform continuous distribution of the distant adsorbed particles is assumed are further given for comparison. The second method, which surpasses the first, is compared with Kirkwood's method. in the case of hexagonal lattice with neighbour interaction. Numerical work is also carried out in this case.

本文就王竹溪先生之理论用两种不同方法加以改良。一种为改变能量公式,另一种为改变中心格点之或然率。用此二法皆可求得近似配分函数。所得关於方格在偶极作用情形下之粘附等温曲线及粘附之数值用图比较之,并与旧日平均连续分布之理论比较。本文所用之第二法实较第一法为佳,故应用之以讨论一三角格在相邻作用情形下之粘附现象,且应用Kirkwood理论以为比较。数值结果亦有图表之。

This paper deals with a method of treating problems of Turbulence from a kinetic point of view. Turbulence "temperature", "pressure", and "entropy" are first defined as state functions, and then the pressure and temperature are incorporated into the equations of motion. Turbulent flows through a circular pipe and between parallel planes are considered in some detail, while the problems of turbulence decay, turbulence structure, and correlation characteristics are briefly discussed. Practically in all cases,...

This paper deals with a method of treating problems of Turbulence from a kinetic point of view. Turbulence "temperature", "pressure", and "entropy" are first defined as state functions, and then the pressure and temperature are incorporated into the equations of motion. Turbulent flows through a circular pipe and between parallel planes are considered in some detail, while the problems of turbulence decay, turbulence structure, and correlation characteristics are briefly discussed. Practically in all cases, the constancy of the turbulence temperature is found to play an important role.

本文系用性论之观点研讨激流之各项问题。先规定激流之情态函数,如温度压力,熵等,然後将激流温度纳入运行公式内,以求得流速之分布,激流之构造与消灭等情形。自各方面观之,本文之理论结果,大都与事实相符。

The phenomellon of limiting heating is of vital importance and interest in the study of gas' flow through a tube with heat additioll fi.om both theoretical and practical points of view. In particular, it has applications to the design of thel.mal ducts of pl'opulsive devices for high speed aircraft. TI}ils poper col,sists of a prelimillary "study Of limiLing'heating for the;(jfole case of a perfect gas in steady flow through a tube of unifornl cross section. It starts from tile fulldamelltal laws governing...

The phenomellon of limiting heating is of vital importance and interest in the study of gas' flow through a tube with heat additioll fi.om both theoretical and practical points of view. In particular, it has applications to the design of thel.mal ducts of pl'opulsive devices for high speed aircraft. TI}ils poper col,sists of a prelimillary "study Of limiLing'heating for the;(jfole case of a perfect gas in steady flow through a tube of unifornl cross section. It starts from tile fulldamelltal laws governing the gas now, fi-om which analytical condiLion for limiting heatillg is then derived, and the beavior of gas at exit as resulted. from limiting heating is discussed in some details. Among the conclusions thus obtained, it is interesting to notice that, as the result of limiting hear,ing the gas is leaving tile exiL with less temperature or velocit,y within certain ranges of initial Mach Number; and that sonic s'tate is 'the limiting state that could be reached by ally flow, subsonic or supersonic, t}lrough 11eat addition.

管内稳流气体之加不能超过一定之限度,逾限即发生所谓限塞现象.在气体动力学之理论与实际上,极限加为一重要而饶有兴趣之问题.在现代高速度航空推进机管部份之设计大多应用。本文试就极限加作初步之分析:篇首先述气体流动之基本定律,由此以诱导加限度公式,再由此讨论气体经过极限加後之状态,并就气体加前之流速分次声速(subsonic),声速(sonic)与超声速(supersonic)三种情况加以比较.在本文所得结论中,有值得吾人注意者即流动气体在某一速度范围之内其温度与速度反因加而减低.此外声速状态(sonic state)为任何流动,(flow),不论是超声速底或次声速底,经加後所能达到之极限状态,亦由本文根据极限加之理论加以证明.在 paul Ghambre与林家翘两先生之“On the steady Flow of a Gas Through aTube with Heat Exchange orchemical Reaction”文中会有仝样之结论,共立论系从气...

管内稳流气体之加不能超过一定之限度,逾限即发生所谓限塞现象.在气体动力学之理论与实际上,极限加为一重要而饶有兴趣之问题.在现代高速度航空推进机管部份之设计大多应用。本文试就极限加作初步之分析:篇首先述气体流动之基本定律,由此以诱导加限度公式,再由此讨论气体经过极限加後之状态,并就气体加前之流速分次声速(subsonic),声速(sonic)与超声速(supersonic)三种情况加以比较.在本文所得结论中,有值得吾人注意者即流动气体在某一速度范围之内其温度与速度反因加而减低.此外声速状态(sonic state)为任何流动,(flow),不论是超声速底或次声速底,经加後所能达到之极限状态,亦由本文根据极限加之理论加以证明.在 paul Ghambre与林家翘两先生之“On the steady Flow of a Gas Through aTube with Heat Exchange orchemical Reaction”文中会有仝样之结论,共立论系从气体瞬间状态之分析入手,不涉加限度.本文则从气体起始与终结状态间之关系着手,而以极限加为讨论中心.如与二氏原文参看可以相中互印证补充。

 
<< 更多相关文摘    
图标索引 相关查询

 


 
CNKI小工具
在英文学术搜索中查有关热—的内容
在知识搜索中查有关热—的内容
在数字搜索中查有关热—的内容
在概念知识元中查有关热—的内容
在学术趋势中查有关热—的内容
 
 

CNKI主页设CNKI翻译助手为主页 | 收藏CNKI翻译助手 | 广告服务 | 英文学术搜索
版权图标  2008 CNKI-中国知网
京ICP证040431号 互联网出版许可证 新出网证(京)字008号
北京市公安局海淀分局 备案号:110 1081725
版权图标 2008中国知网(cnki) 中国学术期刊(光盘版)电子杂志社