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1)  Slat surface
缝翼翼面
2)  wing slot
翼缝
3)  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。
4)  airfoil surface
翼面
1.
Direct measurement system of pressure distribution on airfoil surface using micro pressure sensor array;
基于微型压力传感器阵列的翼面压力分布直接测量系统
5)  upper surface aileron
上翼面副翼
6)  airfoil section
翼剖面;翼型
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。
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