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1)  wake distortion
尾迹畸变
1.
Experiments of rotor wake distortion in pitching maneuvers;
机动飞行中旋翼尾迹畸变效应实验
2.
To improve the prediction of the rotor s off-axis aerodynamic response,the wake distortion effect of maneuvering rotor was studied with the introduction of time-accurate wake curvature parameter(KR) into the maneuvering rotor model.
为改善对旋翼空气动力他轴响应的预测,在旋翼气动模型中引入时变的尾迹弯曲参数KR,以体现机动旋翼的尾迹畸变效应。
3.
A general dynamic,distortional wake model based on the nonlinear and unsteady Peters-He inflow model was investigated and applied to the real-time wake model,it was an important part in the forward acceleration flight because the wake distortion effect and the blade unsteady aerodynamics relation to the whole aerodynamic force.
建立了带吊挂载荷的直升机飞行动力学模型,其中旋翼诱导速度场计算采用了广义动态入流理论模型并添加了畸变项,用以考虑从加速过程的尾迹畸变和附加非定常效应;旋翼气动载荷模型采用了翼型大角度范围插值技术,并结合经典薄翼型理论建立综合的非定常气动载荷模型。
2)  track distortion
径迹畸变
3)  distortion tail
畸变的波尾
4)  wake [英][weɪk]  [美][wek]
尾迹
1.
PIV measurements in the wake of coaxial-rotor in water tunnel;
共轴式双旋翼尾迹流场的水洞PIV测量
2.
A comprehensive method for the generation of constant vorticity contours wake;
等环量线旋翼尾迹生成的广适性方法
3.
Coherent structure in wake over slotted bluff body;
开缝钝体尾迹的拟序结构
5)  wakes [英][weik]  [美][wek]
尾迹
1.
Application of chaos dynamics to the research on plasma wakes;
混沌动力学方法在等离子体尾迹流场研究中的应用
2.
Effects of non-axisymmetric IGV wakes on a low speed axial compressor
非轴对称导叶尾迹对低速轴流压气机的影响
3.
A close relationship between a ship s length and its wakes is presented, and a model is built up based on it.
通过研究尾迹波谱的周期特性与舰船外形特征之间的关系,建立基于波谱函数的舰船长度估计模型。
6)  wake [英][weɪk]  [美][wek]
尾流尾迹
补充资料:飞机尾迹

[[飞机尾迹]]:飞机飞行中发动机排出的废气与周围空气混合凝结而成的特殊的云。一般发生在气温低于-40度、又有适当湿度条件的空气层中。飞机尾迹对飞行没有影响,但暴露行踪,对航空兵战斗行动有一定的影响。

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