2) blade tip clearance
叶顶间隙
1.
Analysis of the flow through the blade tip clearances of axial pumps by CFD;
轴流泵叶顶间隙流动的计算流体动力分析
2.
Optimization design of turbine blade tip clearance shapes
涡轮叶顶间隙形态的优化
3.
The results of the study indicate that the blade tip clearance will lead to a flow blockage at the top zone and increase the separation loss at that zone.
结果表明:动叶叶顶间隙会造成顶部区域的通流阻塞并加重顶部分离损失,根部倒角会减小根部的气流折转角,降低做功能力,而且扩大根部分离区,减小根部流量,增大根部分离损失,因此为了提高数值模拟的准确性应考虑动叶叶顶间隙和根部倒角。
3) Tip clearance
叶顶间隙
1.
3-D numerical analysis of the tip clearance of an aero-engine high pressure turbine;
某型航空发动机高压涡轮叶顶间隙三维数值分析
2.
Numerical analysis of the secondary flow and tip clearance leakage loss
二次流与叶顶间隙损失的数值研究
3.
Numerical analysis of high pressure turbine tip clearance variation
高压涡轮叶顶间隙变化的数值分析
4) blade tip clearance
叶顶间隙叶梢间隙
6) blade tip gap shapes
叶顶间隙形态
补充资料：搅拌器浆叶和流型
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