English translation for "trajectory model"

轨迹模式

Related Translations:

trajectory:  n.(抛射体的)轨道，弹道；流轨；【几】轨线。 a curved [direct-fire, flat, highangle fire, low] trajectory 曲射[直射、平射、高射、低射]弹道。

ejection trajectory:  弹射轨迹

lofted trajectory:  过高弹道

selenocentric trajectory:  月心轨迹

return trajectory:  返回轨道

predicted trajectory:  预计弹道

actual trajectory:  实际弹道实际轨迹

trajectory dispersion:  偏离设计轨迹

computed trajectory:  计算弹道

trajectory height:  弹道高

Example Sentences:

	1.	Standard practice for development and use of oil - spill trajectory models 漏油弹道模型的开发和使用的标准操作规程
	2.	Application of stochastic trajectory model to nozzle two - phase flow calculation 随机轨道模型在喷管两相流计算中的应用
	3.	Particle velocity pdf particles trajectory model of two - phase flow and numerical simulating 颗粒速度概率密度分布轨道模型及数值模拟
	4.	The theory and parameter estimation method to stochastic trajectory models based on phoneme 音素基随机轨迹模型的理论机制和参数估计方法
	5.	This research explores two major fields of flight dynamics first , this research explores the missle scheme trajectory design , trajectory model construction and scheme feasibility , , and the same time a software was supplied which can design proposal trajectory and evaluate particle trajectory through three - degree - of - freedom trajectory simulation 本文着重于对这部分理论进行软件仿真实现和讨论，并在理论和实现上进行了有益的探讨。首先，给出了质点弹道(方案弹道)的数学模型，结合空地导弹给出了导弹飞行的各个阶段的方案。
	6.	In this thesis , based on pershing ii surface to surface missile , a new kind of ballistic missile was designed with an additional rocket engine , which can be ignited twice . firstly , aerodynamic computational models of missile body and warhead which reentry with supersonic are built according to the task requirements ; secondly , the propulsion system model of missile is built whose first two stages are solid rocket engines and the third stage is liquid - solid combined rocket engine . the nozzle and the shape of the engine are designed to meet the needs of the populsion project ; thirdly , the trajectory model of the mass point is built and a wavy trajectory is designed & optimized ; finally , the ability of a missile ' s breaking through defence is analyzed 以美国潘兴导弹为原型，增加可两次点火的末级发动机，改装成具有跳跃能力的地地弹道导弹；首先，根据任务需求，建立了导弹的气动模型，并建立了弹头再入时高超声速气动模型；其次，建立了导弹推进系统模型，前两级采用了固体火箭发动机，第三级采用了固?液组合火箭发动机，并在总体方案要求下，对发动机喷管和外形进行了设计；第三部分，建立了导弹质点弹道模型，设计了一条跳跃式弹道，并对跳跃式弹道进行了优化设计；最后，对导弹进行了突防能力分析，从分析的结果可以看出，跳跃式弹道的突防能力比常规的抛物线弹道要强。
	7.	C . based on a lot of referenced documents and tunnel experiment data , the phenomenon of lateral jet interception are analyzed , and the diagrams of the interaction factor " kcn " is presented . following , the airdefence missile model , trajectory model including attitude - control direct lateral force are constructed 3 、根据大量参考文献和试验数据，分析了侧向喷流的干扰特性，并给出不同状况下干扰因子k _ ( cn )的变化曲线，在上述工作的基础上，建立了带有姿控侧向力装置的防空导弹模型和弹道计算模型。
	8.	( 1 ) the cfd model for the pulse combustion spray drying process . the computational fluid dynamics ( cfd ) based on the two - phase flow theory was employed in this paper , which used the standard k - e model and the particle trajectory model to simulate the gas - particle flow in the drying chamber . the momentum , heat and mass transfer regarding both gaseous and particulate phases during the spray drying inside the drying chamber was also revealed 为解决这一难题，本文利用气体一颗粒两相流理论和计算流体力学( cfd )技术，建立了更符合实际喷雾干燥过程的数学模型即喷雾干燥的cfd模型，并进行了脉动燃烧喷雾干燥过程模拟，其主要内容如下： ( 1 )建立了脉动燃烧喷雾干燥的cfd模型该数学模型建立在气体一颗粒两相流基础之上，用标准k -模型预测干燥室内的气体湍流运动过程，颗粒轨道模型追踪干燥室内颗粒群的运动轨迹，热质传递模型描述空气和液滴的热质传递过程。
	9.	The cause ( s ) and characteristics of vehicle rollover accident are analyzed , the general theory and method are given on reconstruction analysis of this kind of accident . the ‘ three phases ’ theory of vehicle rollover reconstruction analysis is put forward , which are pre - trip phrase , trip phrase and post - trip phrase , adopting relevant theory models , experiential formula and trajectory model in reconstruction analysis . on the basis of certain assumptions , several dynamics and kinematics models describing the vehicle rollover process are established , and the functions between cvs and impact time , impact height or other parameters are gained . then the 基于以上研究背景和社会需求,本文在国内外现有研究成果的基础上,对汽车滚翻事故再现分析的一般理论和方法进行研究,拟定应用于实际汽车滚翻事故再现分析的一般流程、算法和规则,建立了滚翻轨迹模型,开发了滚翻事故再现分析模块( car - rar ) 。
	10.	On the basis of solving ballistic equation in real - time , the authors solved the unified calculation problem of non - flat trajectory comprehensive coefficient under the condition of strong constraint , found the estimating method of flat trajectory comprehensive coefficient , carried out the generalized design of solving trajectory model in real - time , and given a program flawchart 摘要根据基于弹道方程的实时解算算法，解决了强约束条件下非低伸弹种弹道综合系数的统一计算问题，找出低伸弹种弹道综合系数的估计方法，进行了弹道实时解算模型的通用化设计，给出了程序流程并进行了测试。

Similar Words：

"trajectory influence" English translation, "trajectory information" English translation, "trajectory level" English translation, "trajectory measurement" English translation, "trajectory method" English translation, "trajectory of bomb" English translation, "trajectory of boulder fall" English translation, "trajectory of climb" English translation, "trajectory of cyclone" English translation, "trajectory of electron" English translation