1) internal elastic lamina
内弹性膜
1.
Results:With age,the follwing changes happened:the number and the protruding folds of the internal elastic lamina reduced;the content of the elastic fibers decreased significantly( P <0.
结果 :随着年龄增加 ,内弹性膜折叠的幅度和数量均减小 ,弹性纤维含量显著减少 (P <0 。
2) interior ballistic
内弹道
1.
Calculation of launch dynamics with two-phase flow interior ballistic model for self-propelled artillery;
考虑两相流内弹道的自行火炮发射动力学计算
2.
A high-resolution numerical simulation of twophase flow interior ballistics of the weapon with non traditional structure;
非常规结构武器两相流内弹道的高精度数值模拟
3.
Experiment and Numerical Simuliation on Interior Ballistics of Solid Traveling Charge;
固体随行装药内弹道实验及数值计算
3) interior ballistics
内弹道
1.
Design of interior ballistics test system based on LabWindows/CVI;
基于LabWindows/CVI的内弹道测试软件系统的设计
2.
Optimization Design for the Interior Ballistics of Railgun;
电磁轨道炮内弹道优化设计
3.
To provide precise boundary condition for the composite tube heat transfer analysis,this paper adopts one-dimensional flow field model of interior ballistics in bore,and reckons the model of composite tube to be an unsteady quasi-one dimensional flow one,which includes the friction and heat transfer between gas and tube and radial heat conduction inside the tube.
为了给复合材料身管传热分析提供较为精确的边界条件,采用一维内弹道膛内流场模型,将弹后空间核心流部分考虑为包含气流与身管管壁发生摩擦和热交换的不稳定准一维流,得到身管内侧不稳定、非定常可压缩流的边界层方程。
4) interior ballistics
内弹道学
1.
After clarifying the concept and correlation of several velocities, the existent problems of interior ballistics and development directions of interior ballistics research were brought forward.
在澄清若干概念基础上,给出了各速度量之间的确切关系,分析了以往内弹道学的不足,指出了内弹道学研究的努力方向。
2.
Based on the classical theory of interior ballistics, the model of this device is built.
以某种新型的燃气式活塞弹射机构为研究对象,运用经典内弹道学理论分析了整个弹射过程,建立了弹射机构的数学模型,并对该数学模型进行仿真。
3.
On the basis of the lumped physical-mathematical model of interior ballistics given in reference 1,this paper gives a detailed discussion about the conditions leading to the formation of pressure plateau in the combustion chamber of a RLPG,and derives the analytical relationship between the jet area and other parameters under which the pressure plateau can be formed.
在文献1建立的RLPG集总参数内弹道学数学物理模型的基础上，对RLPG压力平台产生的条件进行了详细的探讨，推导了满足压力平台的喷孔面积与膛内其它参量之间的解析关系式，编制了计算程序，处理了计算过程中所产生的压力振荡问题，获得了工程设计中实用的产生压力平台的中心杆半径与其行程的变化关系曲线。
5) Spring
管内弹簧
6) internal ballistics
内弹道
1.
The influence of structure axial vibration on the internal ballistics of solid rocket motor was investigated.
文中研究了固体发动机结构的轴向振动对燃烧室内弹道性能的影响。
2.
The internal ballistics of nozzleless SRM differs greatly from the general motors due to the speciality of its structure.
由于无喷管发动机结构的特殊性,导致其内弹道与传统的发动机产生了较大的差异。
3.
Determination of the bore maxi-pressure point is an important link in solution of internal ballistics zero dimension model.
最大膛压点的确定是内弹道零维模型求解的一个重要环节,传统的优选方法存在着可能陷入局部极值点的问题。
参考词条
补充资料：子宫内膜癌腔内放射治疗
子宫内膜癌腔内放射治疗
子宫内膜癌腔内放疗有：①传统方法，使用治疗子宫颈癌的治疗容器，如宫腔管及阴道容器，(容器有：斯德哥尔摩盒式、巴黎弓形、曼彻斯特卵圆形、北京型等)。其缺点是子宫角部受量不足；②Heyman倡导宫腔填充法，将含有镭或其他同位素的金属小囊填满于子宫腔内，使宫腔各壁均能得到高剂量照射，可使单纯放疗效果由30%～40%增至60%以上；③腔内后装放射治疗。剂量：现在采用高剂量率及中剂量率，摒弃低剂量率。高剂量率：Ⅰ期：A点(位于子宫旁三角区内，代表宫旁正常组织受量)总剂量36～40Gy，F点(位于宫腔放射源的顶端旁开子宫中轴2cm，代表肿瘤部受量)总剂量40～45Gy。腔内治疗分5～6次进行，每周1次，每次剂量大致相同。Ⅱ期～Ⅲ期：A点及F点总剂量均为45～50Gy，腔内治疗分6～7次，每周1次，每次剂量大致相同。中剂量率：Ⅰ期：A点总剂量率45～50Gy，F点总剂量50～55Gy，腔内治疗6～8次，每周1次，每次剂量基本相似，Ⅱ～Ⅲ期：A点及F点剂量均为55～60Gy，腔内治疗7～8次，每周1次，每次剂量大致相同。腔内照射多用137Cs、60Co等。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。