1) disc-wing
碟翼
1.
CFD(computational fluid dynamics)simulations,carried out about permalloy magnetic actuator s influence on vortex and pressure distribution on the upper surface of disc-wing,show that it s control capability is suitable.
介绍了微电磁致动器的工作原理和结构工艺,研究微型碟形飞行器周围特殊的空气流场,在碟翼的翼缘安装MEMS微致动器阵列,扰动边界层分离,从而打破飞行器的空中姿态平衡性,达到控制其进行翻转和俯仰等空中动作的目的。
2.
Micro electromagnetic actuator array for aerodynamic control of the disc-wing has been explored in this paper.
本文以用于控制碟翼边界层流动的电磁式微致动器为研究对象,结合空气动力学和边界层理论分析研究了碟翼的基本气动特性,确定碟翼边界层分离位置,制定出合适的微致动器致动方案。
3) HDD Hard Disk Drive
碟碟机
4) wing
[英][wɪŋ] [美][wɪŋ]
翼
1.
Noise reduction mechanism of non-smooth leading edge of owl wing;
鸮翼前缘非光滑形态消声降噪机理
2.
The wings of projectile provide the lift, control the direction and keep the stability of flying.
翼起到提供升力、控制飞行方向、实现稳定飞行等作用。
3.
Based on CFD technique,three different shapes rudder/wing were designed which consulted some rudders/wings of Autonomous Underwater Vehicles(AUV)mother models.
基于CFD技术,以某水下机器人舵翼为母型,设计了3种不同外形的舵翼。
6) disk spring
碟簧
1.
Development of CAD/CAM integrated system of the disk spring based on AutoCAD R12;
基于AutoCADR12平台下的碟簧CAD/CAM集成系统的开发
2.
The dynamic characteristics of disk spring taking account of effect of static load,nonlinear restoring force and combined Coulomb and viscous damping are presented.
详细研究了考虑静力载荷影响、具有弹性非线性和 Coulomb摩擦阻尼非线性的碟簧元件的动力学特性。
3.
Failure analysis for a cracked disk spring was carried out through chemical composition analysis,hardness test,metallograph observation,fracture analysis and EDAX.
通过对断裂碟簧的化学成分、硬度、金相、扫描电镜和能谱分析,指出了非金属夹杂物,特别是硫化物含量偏高,以及严重的带状组织,阻断了组织的连续性,是产生裂纹的主要原因。
补充资料：变后掠翼飞机(见后掠翼飞机)
变后掠翼飞机(见后掠翼飞机)
swing-wing aircraft
bianhoul位eyi feiii变后掠翼飞机(swing一wing aircran)见后掠翼飞机。
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