词语屋>英语词典>empennage翻译和用法

empennage

英

美

n.  尾翼;尾翼面;尾部; 缩写词为EMP

复数:empennages 

英英释义

noun

双语例句

  • Effectively Analyzing Aeroelastic Model Empirical Design for Empennage Non-Lift Type Buffeting and Its Wind Tunnel Test Data
    尾翼气动弹性抖振模型设计与抖振试验研究
  • The research purpose of this paper is to analysis the flight dynamic performance for unmanned aerial vehicle ( UAV) without empennage and to evaluate its operation and stable performance. Then offer some reference to design and development.
    本文的研究目的是对无尾式无人机的飞行动力学特性进行分析研究,初步评价其操纵与稳定性能,从而为飞机的设计与研制提供一定的参考。
  • Numerical Simulation Study of Performance of Empennage Forming of Liner with Five Concave Arc Margins Cutted
    五凹弧切边罩尾翼成形三维模拟研究
  • Based on test and simulation of aircraft windshield, the anti-bird impact design guide line of aircraft typical structures for radome and leading edge of wing and empennage is discussed.
    最后在对飞机典型结构风挡、雷达罩、机尾翼前缘的试验与仿真研究的基础上,对飞机典型结构的抗鸟撞设计准则进行了探讨。
  • Utilizing the functions of CATIA software in Reverse Engineering deals with point cloud data of mobile empennage that is gained from laser measuring and reconstitute the curved surface. Gains the solid model that Rapid Prototyping requires.
    在逆向工程中应用CATIA软件处理激光测量的方法得到的汽车尾部局部点云数据,进行曲面重构,获昨快速原型所需的实体模型。
  • The utility model relates to a toy plane which is composed of a plane body, wings, an empennage, an electric machine, batteries, propellers, a driving device, direction wheels, etc.
    新型空陆玩具飞机,由机身、机翼、尾翼、电机、电池、螺旋桨、传动装置、方向轮等组成。
  • Study on Isothermal Forming Technology for Complex Empennage
    复杂尾翼等温成型工艺研究
  • The modeling of rotor unsteady aerodynamics and rotor/ fuselage/ empennage aerodynamic interaction have been the bottleneck in the high-fidelity mathematical modeling of helicopter flight dynamics.
    旋翼非定常气动力建模以及旋翼与直升机其它部件的气动干扰建模一直是影响直升机飞行动力学数学模型置信度的瓶颈。
  • Related basic theory of the algorithm is elaborated. The bird strike simulation research on aircraft typical structures such as radome and leading edge of wing and empennage are conducted too and meaningful conclusions was obtained.
    本文系统阐述了该算法的基础理论,并利用SPH算法对飞机典型结构雷达罩、机尾翼前缘模型进行了鸟撞仿真研究,得到了很有意义的结论。
  • The moveable horizontal surface of the empennage used for pitch trim.
    飞机尾翼的可动水平面,用来控制俯仰配平。