1) root stall
翼根失速
2) wingtip stalling
翼尖失速
1.
Characteristics of tailless aircraft wingtip stalling, including common and unique characteristics compared with other configurations, are analyzed with emphasis placed on the effect of wingtip stalling on flying qualities of tailless aircraft.
首先分析了无尾飞机翼尖失速的特点 ,包括与其他布局形式共有的和自身特有的特点 ,重点是翼尖失速对无尾飞机飞行品质的影响。
3) hydrofoil stall
翼型失速
1.
The electromagnetic force provides with the effective affects for increasing the lift forces of the hydrofoil and reducing drag and controlling the hydrofoil stall.
电磁场在导电的流体边界层上产生的电磁力能有效地改变边界层的结构,控制边界层的流动分离,消除涡流,可以增加翼型体升力,减少其阻力,实现对翼型失速的控制。
4) rotor blade stall
旋翼失速
6) airfoil stall
薄翼翼型失速
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