1) converting velocity
转捩速度
1.
The experimental results show the rails have slighter damage with high velocity and low armature voltage of 50-100V, converting velocity is different because of its initial velocity for the SA, and the energy deposited in the SA in the bore can be reduced significantly.
在分析固体电枢结构和电热特性基础上进行了设计与实验，实验结果表明，在高速时导轨有轻微烧蚀，电枢弧压很低为５０～１００Ｖ，并由于初速不同转捩速度亦不同，电枢耗能显著降低，故提高了发射效率并降低了烧蚀。
2) transition length
转捩区长度
1.
The author modified the Abu-Ghannam and Shaw Transition Model (AGS Transition Model) with ready test data,set out the concept of calculating the transition length with arc Reynolds number and compared the calculated value with the test value.
本文作者利用现有的试验数据对Abu -GhannamandShaw〔1〕转捩模型 (AGS转捩模型 )进行了修正 ,提出了利用弧长雷诺数模型确定转捩区长度的思想 ,并对计算结果与试验值进行了比
3) transition
[英][træn'zɪʃn] [美][træn'zɪʃən]
转捩
1.
Visualization study on the flow structures in the transitional boundary layer under an adverse pressure gradient;
逆压梯度转捩边界层流动结构显示
2.
Study of bypass transition mechanisms in the boundary layer of blunt bodies;
钝体头部边界层“逾越”型转捩机理研究
3.
Improving the aerodynamic performance of low Reynolds number airfoils in oscillating freestream with forced transition method;
固定转捩在改善振荡来流下低雷诺数翼型气动性能中的应用
4) hypersonic boundary layer transition
高超声速边界层转捩
1.
Several fundamental research topics are discussed for future research,which in- clude the advanced hypersonic test facilities;modeling aero-thermo-chemistry;stagnation flow region prediction; hypersonic boundary layer transition and shock waves/viscous interactions.
回顾了高温气体动力学与高超声速科技相关的一些重要研究进展,探讨几个具有基础性研究意义的方向：即高超声速流动模拟；高温气体热化学反应机制；高超声速流动滞止区预测；高超声速边界层转捩和激波/激波相互作用诱导的气动热问题。
5) Transition process in a hypersonic boundary layer
高超音速边界层转捩
6) twisted length
一次风边界转捩长度
1.
The twisted length has been defined.
对一次风边界转捩长度b进行了定义,分析了一次风边界转捩长度的影响,并对其变化规律进行了研究,为同轴旋转分层流燃烧器分层机理的研究打下了基础。
补充资料：捩转
1.掉转;扭转。
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