倾转旋翼,tiltrotor英语短句,例句大全

倾转旋翼,tiltrotor
1)tiltrotor倾转旋翼
1.Modeling and analytical investigation on rotor/wing aerodynamic interaction for tiltrotor aircraft;倾转旋翼机旋翼对机翼气动干扰的建模及分析
2.Calculated method and parametric effect investigation of wing download of tiltrotor aircraft;倾转旋翼机机翼向下载荷的计算方法及参数影响分析
3.Experiment on aeroelastic characteristics of tiltrotor aircraft in transition flight;倾转旋翼/机翼耦合系统过渡状态气弹动力学试验研究

英文短句/例句

1.Calculation of the Aerodynamic Interaction between Rotor／Wing／Fuselage of Tilt-Rotor;倾转旋翼飞行器旋翼/机翼/机身气动干扰计算
2.Review of Aeroelastic Stability Investigations for Tiltrotor Aircraft倾转旋翼机气动弹性稳定性研究进展
3.Modeling study on tilt-rotor's aeroelastic stability in cruise flight前飞状态倾转旋翼机气弹稳定性建模
4.Bell/Boeing 609--First Civil Tiltrotor贝尔/波音609民用倾转旋翼飞机——民用飞机的新葩
5.Study on Some Aeroelastic and Stability Analyses of Tiltrotor;倾转旋翼机气弹响应及稳定性若干问题研究
6.Design and Realization of the Servo System for Tiltrotor Model Bench;倾转旋翼模型实验台伺服系统设计与实现
7.A Mathematical Model of Tilt-rotor Flight Dynamics and Investigation of Flight Control in Transition Mode;倾转旋翼飞机过渡模式动力学建模与控制研究
8.Research on Application of the Virtual Prototyping Technology to Tilt-Rotor Design;虚拟样机技术在倾转旋翼设计中的应用
9.Research on Tilt Rotor Vertical Take-Off and Landing Roll Channel Control Problem;倾转旋翼机垂直起降滚动通道控制问题研究
10.Research of Dual Model Reference Adaptive Control System for Tilt-Rotor Aircraft倾转旋翼机模型参考自适应双重控制系统研究
11.Design and Research of Control law for TiltRotor in Transition Flight Phase倾转旋翼机过渡飞行阶段控制律设计研究
12.Full Envelope Flight Control Method for Small Unmanned Tilt Rotor Aircraft小型无人倾转旋翼机全模式飞行操纵控制
13.Design of Flight Control System for a Small Unmanned Tilt Rotor Aircraft小型无人倾转旋翼机飞行控制系统设计(英文)
14.Computational analysis on tiltrotor aerodynamic characteristics for transitional flight过渡状态的倾转旋翼气动特性计算分析(英文)
15.Control Strategy for Tilt-Rotor Aircraft Trimming in Steady Level Flight倾转旋翼飞行器的操纵策略和配平方法
16.A Mathematical Model of Unmanned Tiltrotor Aircraft and Research on Attitude Control System Design;无人倾转旋翼机飞行力学建模与姿态控制技术研究
17.Design of Operation Unit and Its Control System for Tiltrotor Model Bench;倾转旋翼模型实验台的操纵机构及控制系统设计
18.A Method of Stability Evaluation of Tiltrotor in Helicopter Mode倾转旋翼机直升机状态系统稳定性判断的一种方法

相关短句/例句

tilt rotor倾转旋翼
1.Multidisciplinary design optimization for aerodynamics/structural dynamics of tilt rotor blade;倾转旋翼桨叶空气动力学/结构动力学多学科优化设计研究
2.Considering the operational characters of tilt rotor/propeller,a design method for tilt rotor/propeller is presented.针对小型倾转螺旋桨独特的工作特性,在研究国外有关倾转旋翼桨叶设计现状的基础上,本文运用了遗传算法对桨叶的参数进行了寻优设计分析,以满足不同飞行状态的性能要求。
3.The new-concept variable diameter tilt rotor (VDTR) which has a combined aerodynamic advantage of a large-diameter rotor in hovering flight and a small-diameter rotor in cruise flight represents a key developmental direction of the tilt rotor.新概念变直径倾转旋翼综合了悬停时大尺寸旋翼和巡航时小尺寸旋翼的气动优点,是倾转旋翼飞行器的一个重要发展方向。
3)tilt-rotor倾转旋翼
1.<Abstrcat> In the present paper, the rotor wake of tilt-rotor aircraft is classified into the steady wake in hover and forward flight and the unsteady wake in transition flight, and a rotor free-wake analytical method for tilt-rotor aircraft has been developed based upon the Weissinger-L lifting-surface theory and rolled-up tip vortex model.将倾转旋翼机的旋翼尾迹问题区分为二类,即悬停和前飞等状态的定常尾迹以及过渡飞行状态的非定常尾迹。
2.In this paper, the aerodynamic interactions between rotor/wing/ fuselage of tilt-rotor in hover and transition flight was calculated.本文计算了倾转旋翼飞行器悬停状态和过渡飞行状态的旋翼/机翼/短翼/机身之间的气动干扰和气动特性,分析了其特点,并进行了初步的试验验证。
3.This thesis is aimed at the interaction aerodynamics problem on the rotor flowfield of a helicopter and a tilt-rotor aircraft by applying the rotor vortex theory and the panel method, and the major contributions of the author s research work are as follows:Based on the blade Weissinger-L model, rotor roll-up tip vortex model .本文采用涡流理论方法和面元方法，对直升机和倾转旋翼机的旋翼下洗流场的干扰空气动力学问题进行了较为深入的研究。
4)tiltrotor倾转旋翼机
1.The parameter uncertainty in tiltrotor model caused by the variation of nacelle angle was considered in controller designing for flight mode conversion of tiltrotor.针对倾转旋翼机过渡段模型参数摄动问题,在状态方程描述的框架下,用线性分式变换形式将模型参数摄动表示为对角块结构,采用μ综合方法设计了倾转旋翼机过渡段飞行控制器。
2.The airplane mode s model of tiltrotor was founded.建立倾转旋翼机飞机模式的分析模型,分析系统的频率和阻尼特性,揭示了对系统稳定性起主要作用的一些模态;分析了旋翼摆振运动、机翼气动力和自转状态假设对系统稳定性的影响;分析了系统一些重要参数,如桨叶固有频率和机翼固有频率,对系统回转颤振稳定性的影响。
3.The multi-body analysis of the aeroelastic stability of the tiltrotor aircraft is presented.通过多体动力学方法建立了倾转旋翼机动力学分析模型。
5)tiltrotor aircraft倾转旋翼机
1.Dynamic stability analysis of tiltrotor aircraft in forward flight;倾转旋翼机前飞动力学稳定性分析
2.Considering the characteristics of the thrust vector/aerodynamic force multiple control for tiltrotor aircraft, this paper,based on the model of the tiltrotor aircraft, designs the flight control system using variable structure control with sliding mode.文中针对倾转旋翼机拉力矢量/气动力组合控制的特点,在完成倾转旋翼机建模的基础上,采用滑模变结构控制对飞行控制系统进行了设计。
3.In this paper the flight control system of tiltrotor aircraft is designed by using linear model following method to resolve the coupling of lateral channel.文中针对倾转旋翼机横侧向飞行控制系统的耦合问题,应用线性模型跟随法进行控制器的设计。
6)tilt-rotor倾转旋翼机
1.Natural characteristic analyse of the transmission of Tilt-Rotor;某型倾转旋翼机传动系统固有特性分析
2.Dynamic response analysis of the transmission of tilt-rotor in different modes;倾转旋翼机传动系统多状态响应特性研究
3.Modeling study on tilt-rotor's aeroelastic stability in cruise flight前飞状态倾转旋翼机气弹稳定性建模