1) rapidly pitching airfoil
快速上仰翼型
1.
The problem of unsteady separated flow of rapidly pitching airfoil with oscillating motion is computationally studied.
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。
2) pitching airfoil
上仰翼型
1.
The vortex structure shed from the trailing-dege of a constant-rate pitching airfoil was visualized using hydrogen bubble technique.
在尾缘处置氢气泡铂丝,观察了上仰翼型自尾缘流入尾迹的涡层。
3) rapid pitching
快速俯仰
1.
Based on the analysis of typical post-stall maneuvers,steady linear flight,rapid pitching and rolling about velocity vector are presented as three typical basic movements.
对典型过失速机动的运动特性进行了分析,根据其运动特点将过失速机动的运动过程分解为定直飞行、快速俯仰和绕速度矢量旋转三种基本运动的组合。
4) identical pitching
等速上仰
1.
Computationally simulated the dynamic stall about the pitching NACA0015 airfoil with identical pitching rate (α= 0°60°, at Low Reynolds number (Re = 4.
8×104)条件下NACA0015翼型作等速上仰(α=0°-60°)的动态失速过程,同Walker的试验结果比较,验证了计算结果的正确性。
5) rate of pull-up ; negative pitch rate
上仰角速度
6) low speed airfoil
低速翼型
1.
A method for the computation of flow separation andstall on low speed airfoils by viscous-inviscid interaction is presented.
本文用势流－边界层相互作用方法计算低速翼型的分离和失速。
补充资料：仰仰
1.同"昂昂"。 2.气概轩昂貌。
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