For aircraft increase the chances of snow and rain when they take off and land, a study suggests.
研究表明，飞机起降增加了当地下雨雪的几率。
Study after study shows that the price of combat aircraft has been rising substantially faster than inflation, often faster than GDP.
不断有研究表明，战斗机的价格增速已经远远超过通货膨胀的速度，而通货膨胀的速度又常常大于GDP增长的速度。
Concerns about aircraft safety during the eruption of an Icelandic volcano in 2010 were well founded, according to a new scientific study.
通过一项新的的科学研究成果，在2010年冰岛的一座火山喷发期间的飞行器安全问题已经得到关注。
As planes push cloud temperatures past the tipping point at which supercooled water freezes, the aircraft "seed" the clouds with ice particles, the study says.
研究者称，飞机飞行将云温推至临界点以下，为那些过冷的液态水提供了云形成的冰颗粒，使其凝聚冻结。
Some time ago the United States Navy, for instance, examined a very large number of men working on aircraft carriers: the study was known as Project Anehin.
例如，美国海军前些时候调查了许多在航空母航上工作的人，这次调查被称之为：“安内英工程”。
For all of our theoretical study models using X PLANE and MSFS we will rate this total lifting capacity at 25% of the total weight of our aircraft in question.
对于我们的理论学习模式都使用X飞机和无国界医生将会给我们的25我们在有关飞机总重量％的总起重能力。
It is a virtual study in a theoretical whirling winged aircraft.
这是一个在理论旋转翼飞机的虚拟研究。
Is the first to be affected are the National School of Administration study of Xie Yalong, 28, he went to board the aircraft.
首当其冲的是正在国家行政学院学习的谢亚龙，他在28日登上了前往的飞机。
The study of the aircraft carrier battle group (CVBG) communication countermeasure system is a very important problem.
航母战斗群通信对抗系统的研究是一个十分重要的课题。
China USES an aircraft as business the occurrence likelihood of emulative manufacturer throws into confusion the pattern of this group course of study.
中国作为商用飞机竞争性厂商的出现可能打乱这一行业的格局。
The study on spectral and spatial distribution characteristics of infrared radiation of plume is useful for the demand of detection or defense mechanism of aircraft.
对飞机尾焰红外辐射的光谱特性及空间分布特性进行研究，将满足对飞行器探测或防护的需求。
In this paper, a model of statistical energy analysis is used to study sound transmission loss of the aircraft cabin, and predict the sound field in the cabin.
文章建立了飞机壁板隔声的统计能量分析模型，研究了外部声场激励和振动激励通过飞机壁板的隔声量，预测了飞机舱室内的声场分布。
The study will provide a new theoretical approach to investigate aircraft agility, the direct force control and post-stall maneuver of modern combat aircraft.
为飞机敏捷性、直接力控制和过失速机动问题提供了一种理论研究方法。
Through the study on improving of the airtightness of aircraft cockpit, selection and application in a type of aircraft for XM - 17A non-drying putty were introduced.
通过对某型飞机座舱气密性改进研究，介绍了XM-17A不干性腻子的选用及在某型飞机上的应用。
PTAE 4A AE monitor system was developed for monitoring the fatigue crack propagation on aircraft structure. And a study on its practical application was carried out.
为实现飞机结构的疲劳裂纹动态监控，研制了PTAE-4A机载声发射监测系统，并作了随机机载应用研究。
Therefore aircraft fault diagnosis system electromagnetic interference study of great significance.
因此飞机电磁干扰故障诊断系统的研究具有十分重要的意义。
The study of the resistance prediction method is presented with the thin ship theory for USS Enterprise aircraft carrier.
使用薄船理论，针对美国“企业”号航母进行航母阻力理论预报方法的初步研究。
The theory and the methods of study antenna were discussed in detail and combined with some conditions of the MA60 aircraft, illuminating the development plan of the shortwave antenna.
详细地讨论了天线研究理论和方法，结合MA60飞机的实际情况，论证了短波电台隐蔽式天线的研制方案。
Some relative theories for the study of aircraft vulnerability are discussed. Furthermore the method for calculating vulnerability index of aircraft is introduced.
论述了军用飞机易损性研究中的相关理论，并对飞机易损性定量指标的计算方法进行了介绍。
In the study of civil aircraft afterbody test, it's adopted many kinds of afterbody shape models and the model with or without tail.
在民机后体试验技术研究中，采用多种不同后体形状和有无尾翼模型进行试验。
Along with the deep development of study, the microjet technology will be possibly applied to control the aerodynamic flow of the high speed aircraft surface and the thrust vector of rocket engine.
并指出，随着研究工作的深入，该项技术还可望用于高马赫数飞行体表面气体流动控制、火箭发动机推力方向控制等。
Electrical Engineering and Automation tentacles all walks of life, small to a switch designed to study aerospace aircraft, has its shadow.
电气工程及其自动化的触角伸向各行各业，小到一个开关的设计，大到宇航飞机的研究，都有它的身影。
The objective of this paper is to study the effects of three dimensional constraints on fatigue crack growth under aircraft spectrum loading.
研究裂纹端部三维应力约束、塑性约束和位移约束等对谱载疲劳裂纹扩展的影响。
The objective of this paper is to study the effects of three dimensional constraints on fatigue crack growth under aircraft spectrum loading.
研究裂纹端部三维应力约束、塑性约束和位移约束等对谱载疲劳裂纹扩展的影响。
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