2) 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
3) rotor wing
旋转机翼
1.
Development of experimental equipment for reaction driving rotor wing;
尖部喷气驱动旋转机翼地面试验装置的研制
4) revolving wing
旋转翼
1.
In comparison with flapping mode, a little more amount of average lift and better aerodynamic efficiency are obtained by a revolving wing in hovering.
用拟压缩性法求解三维非定常不可压N-S方程,研究了旋转翼及拍动翼的气动力和流场。
5) 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。
6) 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。
补充资料：旋转-旋转式扫描系统
旋转-旋转式扫描系统
影像学术语。CT设备的类型之一。扫描方式为旋转-旋转式(rotate-rotate，R/R)的CT设备。扫描时X线管和排列成扇形的探测器阵列做同步旋转，属第三代CT机，可用于全身CT检查，是70年代后期以来临床应用的主流机型之一。X线管为旋转阳极，发射大角度扇形线束，探测器多为氙气电离室或为固体探测器，阵列规模通常在数百甚至上千。扫描时间1～4秒。通常具有靶扫描、靶重建、动态扫描、三维成像等特殊程序和多种重建算法、测量分析功能。旋转-旋转式设备在扫描过程中探测器是连续工作的，利用率高，但不能同时进行校准。所获取的每一幅投影轨迹剖面图都是由整个探测器阵列同时采集的信息构成的，个别探测器出现误差便可能使反投影后的重建图像上出现环形伪影(ring artifact)。该型机不具备体积采样能力。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条