The applications of the uniform experimental design and Monte Carlo testing method to computational flight mechanics are emphasized.

  • 重点介绍了均匀试验设计法和统计试验法在计算飞行力学中的应用。
  • 来源:互联网摘选更新时间:2026-07-01 16:04:06

  • 重点词汇
  • uniformn.制服;校服;
  • OFabbr.Old French 古法语;
  • applicationsn.(尤指理论、发现等的)应用,运用;申请;请求;申请表;申请书;施用;动用;涂抹;敷用;施用;
  • monten.蒙特;绳索牵引吊斗;一种始于西班牙的纸牌赌博游戏;
  • theart.这个;指已提到或易领会到的人或事物;指独一无二的、正常的或不言而喻的人或事物;用以泛指;与形容词连用,指事物或统称的人;用于姓氏的复数形式前,指家庭或夫妇;(指特定用途的事物)足够,恰好;每,一;当前的,本,此;(重读,表示所指的为知名或重要的人或事物)
  • testing method试验法
  • ofprep. 关于;属于…的;由…制成;
  • experimental design试验设计;
  • 相关例句
1、

Development of computational flight mechanics

计算飞行力学的产生和发展

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2、

So, IAAP is an interdisciplinary-science, which bridges the flight mechanics, aerodynamics, elasticity and cybernetics.

它是处于空气动力学、飞行力学、弹性力学和现代控制论之间的应用性研究课题。

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3、

Flight mechanics in the information age

信息时代的飞行力学

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4、

In this paper, the problem in flight mechanics and aerodynamics for rolling resonance of the re-entry body are discussed;

本文综述了再入体滚转共振的飞行力学和气动力学问题;

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5、

The important roles of experimental design in computational flight mechanics have been discussed;

讨论了试验设计在计算飞行力学中的重要意义;

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6、

Making an example of a high-gain CAS ( Control Augmentation System), this paper deals with the design of main parameters of a CAS and the rela-tion between these parameters and an aircraft flight character, from the angle of flight mechanics.

本文从飞行力学的角度出发,着重以高增益控制增稳系统为主来讨论控制增稳系统的主要参数的设计及其同飞行品质的关系问题。

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7、

A flight mechanics and stable control loop model of interception missile with the blended control by aerodynamic force and moment-gas-thrust-vector

空气动力和直接侧向力复合控制的拦截弹飞行力学及稳定回路模型

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8、

Some Problems of Flight Mechanics in the Improvements of Guided Missile

导弹改进、改型中的飞行力学问题

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9、

Flight Mechanics Towards the 21st Century

迈向21世纪的飞行力学

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10、

In this paper, from the angle of the development of the flight mechanics software system of tactical missiles, the design idea is presented.

从战术弹飞行力学软件系统的设计开发角度,提出了软件系统的设计指导思想。

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11、

The mathematical model of helicopter flight dynamics, which is the research basis of flight mechanics, shows the understanding level for helicopter to a great extent.

根据国内外直升机数学模型研究情况,从飞行动力学的角度分析直升机数学模型的特点。

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12、

Tentative opinion of introducing supersonic flight in mechanics of general physics

在普通物理力学中介绍超音速飞行的设想

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13、

Method of guidance flight mechanics

制导飞行力学方法

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14、

Technique of in flight measurement of pressure distribution on a subsonic transport aircraft is introduced. Some flight test results are presented.

简要地介绍了亚音速飞机压力分布测量的飞行试验技术,并给出了部分试验结果。

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15、

Earth Magnetic Field Sensor and Its Application in Flight Body Attitude Measurement

地磁场传感器及其在飞行体姿态测量中的应用

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16、

According to the characteristics of the load on the canopy, the method for measuring the load on the canopy with a pressure sensor is presented, and then the flight measurement of the load spectrum of the canopy is realized for the first time.

根据活动舱盖载荷特性,提出用压力传感器测量活动舱盖载荷的方法,并首次实现了活动舱盖载荷谱飞行测量。

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17、

In the end, the method is checked with flight test data in measurement noise.

最后,根据有观测噪音的试飞数据对本文方法进行之检验。

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18、

By connecting several data collectors with a single bus, which is the trend of development of flight data measurement, we can improve the data acquisition capacity and flexibility significantly.

在飞行数据采集系统中,采用现场总线技术,可以在一条总线上挂接多个数据采集器,因此显著提高了采集处理能力,增强了使用的灵活性,这是飞行数据测试系统的发展趋势。

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19、

Ultrasonic high-resolution flight-time measurement system

高分辨力超声波飞行时间测量系统

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20、
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