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1)  flap gap
襟翼缝道
1.
Investigation of effect of flap gap on multi-element airfoil aerodynamical characters;
襟翼缝道对多段翼型气动特性影响的实验研究
2)  slotted flap; spoit flap
开缝襟翼
3)  THREE SLOTTED FLAP
三开缝襟翼
4)  leading-edge slat
缝翼缝道
1.
The comparative investigation between the direct measuring method and surface pressure measurement method of the aerodynamics force on airfoil is performed in two-dimensional testing section of NF-3 wind tunnel at Northwestern Polytechnical University;and the experimental investigation of aerodynamics performance of multi-element airfoil with leading-edge slat is carried out.
结果表明,测力和测压两种方法均可用于翼型的实验研究,前缘缝翼缝道的不同构型对多段翼型的增升效果和气动效率(升阻特性)都有极大的影响。
5)  flap [英][flæp]  [美][flæp]
襟翼
1.
Aerodynamic model of airfoil with flap used for electrical controlled rotor aeroelastic analysis;
用于电控旋翼气弹分析的带襟翼翼型气动力模型
2.
Numerical simulation of 2D airfoil lift enhancement with flaps;
二维翼型襟翼增升的数值模拟
3.
Firstly,a synthetic unsteady aerodynamic model in time domain is presented,which can take account of the unsteady effect of the flap nose overhang.
以有限元旋翼气弹分析程序LORA01为基础,首先给出了一种能计及襟翼移轴补偿影响的时域综合非定常气动力模型,并将伺服襟翼作为额外引入的质量体计入结构动力学模型;之后结合有限元法,根据Hamilton原理导出由广义力表示的带襟翼桨叶非线性运动方程,采用基于Newmark方法的隐式数值积分法对桨叶运动方程进行求解。
6)  body flap
机身襟翼
1.
All-C/SiC composites body flap is gas-loaded intensely when the return of the space vehicle into Earth s atmosphere with high-supersonic.
针对全C/SiC复合材料机身襟翼再入过程中受到强烈的气动载荷作用的受力状况,进行了静力试验考核。
补充资料:道-道间寻道时间
道-道间寻道时间(single track seek):  
指磁头从一磁道移动至另一磁道的时间,单位为毫秒(ms)。
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