1) Wind tunnel side wall layer
风洞侧壁附面层
2) sidewall boundary layer
侧壁附面层
3) side wall interference
风洞侧壁干扰
4) end wall boundary layer
端壁附面层
1.
From the analysis of the shape of the end wall boundary layer at the entrance of a rotor blade tip, the discrepancy in the boundary layer, between a linear cascade without end wall motion (denoted here situation No.
通过对动叶叶尖进口端壁附面层的性状分析 ,指出采用平面叶栅模拟动叶叶尖间隙流端壁面静止(工况 1 )和仅有端壁面运动 (工况 2 )进口端壁附面层与真实情况的差异。
2.
The authors in previous papers[1,2] found it necessary to replace 2-dimensional model with3-dimensional model for predicting blade force defect in end wall boundary layer inside axial compressorcascade.
本文基于实验结果,提出了一种预测轴流压气机叶栅端壁附面层叶片力亏损的通用模型。
5) annulus wall boundary layer
环壁附面层
6) vertical sides of opening
洞口侧壁
补充资料：附面层
见边界层。
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