一旦飞机被阻挡了，正确的反应该是减缓上仰并且提高速度。
Once a plane is stalled, the correct response is to lower the nose and increase speed.
对带振荡的快速上仰翼型的非定常分离流问题进行了计算研究。
The problem of unsteady separated flow of rapidly pitching airfoil with oscillating motion is computationally studied.
本文阐述上仰水平轴风力发电机一种过载自动保护特性的工作机理及其应用价值。
This article expounds both the working-mechanism and the application value of the overload auto-protection feature the small Angle elevated horizontal axis type wind-generator.
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