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Home > chinese-english > "aerodynamic interaction" in English

English translation for "aerodynamic interaction"

空气动力干扰
气动互制


Related Translations:
aerodynamic retarder:  空气动力缓速装置气动缓冲器
aerodynamic compressor:  空气动力压缩机
aerodynamic interference:  空气动力干扰气动干扰
aerodynamic holography:  空气动力全息照相术
aerodynamic asymmetry:  空气动力不对称
aerodynamic method:  空气动力的
aerodynamic exciter:  空气动力激发器
aerodynamic shape:  空气动力外形
aerodynamic excitation:  空气动力扰动
aerodynamic maneuver:  利用空气动力的机动飞行气动力操纵
Example Sentences:
1.Experiment study of aerodynamic interactions of projectile with jet from its forebody
弹丸前体喷流的气动力干扰实验研究
2.The rotor / wing aerodynamic interactions of the tilt rotor vehicle in hover is described in this dissertation
本文主要研究的是倾转旋翼飞行器悬停状态时,旋翼机翼之间的气动干扰问题。
3.Taking advantage of hypersonic panel method , the analysis predicts lateral jet aerodynamic interaction for a blunted body in a hypersonic flow
将高超声速面元法用于喷流流场计算,计算结果与试验结果大体一致。
4.Research on the aerodynamic interaction between the rotors and components of rotorcraft have been a very important aspect and a very challenging subject in rotorcraft aerodynamics
旋翼干扰空气动力学问题一直是旋翼飞行器空气动力学的研究热点和难点之一。
5.Furthermore , because rotors are mounted on the tips of the wing , the rotor / pylon / wing aerodynamic interactions are also included in the model . such factors reflect the unsteady and nonlinear characteristics in the model
此外,倾转旋翼飞机的旋翼安装在翼尖,旋翼/发动机短舱/机翼之间的气动干扰是建模的一个难点。
6.Finally , an iterative method coupled between rotor free wake model and lifting wing panel model is given . by the method , the aerodynamic interaction of the rotor on its wing for tilt - rotor aircraft in hover are computed and discussed
最后,建立了一个耦合的旋翼机翼气动干扰分析方法,计算分析了悬停状态旋翼流场对机翼的气动干扰影响。
7.Many factors were considered in the algorithm such as the helicopter nonlinear flight dynamic model , the time delay of rotor wake , the air compressibility at advancing blade , the stall of retreating blade , the unsteady flapping motion of rotor blades and the aerodynamic interaction among rotor , fuselage , tail rotor and empennage
根据这一方法可以确定为完成直升机机动飞行所需的驾驶员操纵输入及直升机的飞行速度、角速度和飞行姿态的变化历程。
8.The investigation of the distribution of aerodynamic forces on the external stores and their neighboring aircraft surfaces during the transient process of the separation of the external store from an aircraft is an urgent need because aerodynamic interactions can cause the released store to impact upon , and possibly damage , the aircraft
从载机上发射导弹、投掷炸弹或抛弃副油箱时,外挂物处于载机复杂干扰流场中。此时往往出现不正常分离,有时会导致外挂物与载机发生碰撞,严重危及载机和飞行人员安全的重大事故。
9.Based on the mechanism of slipstream interaction , described in this thesis is firstly the interaction of the propeller slipstream with the wing 、 fuselage and horizontal tail . subsequently , the changes in lift 、 drag and pitching moment are derived , giving an engineering model for the prediction of the increments in the aerodynamic characteristics caused by the interference between the propeller slipstream and the other parts of aircraft . this method offers a powerful means to the calculation of the aerodynamic interaction between the propeller and the aircraft , providing reliable data for the design of and aerodynamic calculation on propeller - powered aircraft
本文以滑流干扰的机理为出发点,研究了螺旋桨滑流与飞机机翼、机身、平尾组合体之间的相互影响,推导出滑流引起的飞机升力、阻力和俯仰力矩的变化,给出了滑流干扰对机体气动特性影响的工程估算方法,为研究螺旋桨与飞机部件之间的相互干扰提供了有力的工具,为以螺旋桨发动机为动力的飞机的设计和气动计算提供可靠的依据。
10.Along with development of tiltrotor vehicle ’ s research some theoretical productions have been appeared in some project ( aerodynamic behavior of rotor , kinetic behavior of rotor , rotor / wing aerodynamic interactions , etc . ) . in order to carry on further research and experimentation of these project , national - defence science and technology helicopter rotor kinetic lab of our school begin to building tiltrotor model bench . base on need of this bench , this paper study / design pitch control system on it
随着对倾转旋翼飞行器的深入研究,倾转旋翼的气动特性、动力学特性、旋翼/机身间的气动干扰等课题方面已有一定的理论成果出现。为了对这些课题进行深入研究和试验验证,我校直升机旋翼动力学国防科技重点实验室着手建造了倾转旋翼模型实验台。
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