1) Boundary layer suction+
附面层抽吸+
2) boundary layer suction
附面层抽吸
1.
The characteristic features of the concept are made clear through its comparison with the MIT boundary layer suction com- pressor.
结合附面层抽吸+技术提出了低反动度、高负荷轴流压气机的概念。
2.
A numerical investigation about effects of boundary layer suction in low-speed compressor stator cascade with large turning angle was carried out.
本文采用数值方法研究了低速条件下附面层抽吸+对大折转角矩形叶栅流场的影响。
3.
To provide a further prospective of the boundary layer separation of compressor rotor under high load and off-design working conditions,numerical method was used to study the effects of boundary layer suction of compressor rotor at different suction positions and suction flow rates on the aerodynamic performance of rotor.
针对压气机叶片在高负荷及非设计工况下经常出现的附面层分离状况,采用数值方法研究了叶片吸力面不同位置、不同吸气量时附面层抽吸+对压气机转子气动性能的影响。
3) boundary layer suction(BLS) experiment
附面层抽吸试验
4) boundary layer suction
附面层抽吸技术
5) Absorption surface
吸附面
6) boundary layer
附面层
1.
Investigation on Application of Dihedral/Swept Blade and Boundary Layer Suction to Control Vortex Configurations in Compressor Cascades;
采用叶片弯/掠及附面层抽吸+控制扩压叶栅内涡结构的研究
2.
The accurate prediction of drag is key to the design of the low Reynold′s number flight vehicle,and the accurate prediction of friction drag which is induced by separation and transition of the boundary layer is key to the accurate prediction of drag.
而与附面层分离和转捩相关的摩擦阻力的精确计算则是此类飞行器阻力精确计算的关键。
3.
The results show that,the boundary layer suction could reduce the cascade s total pressure losses,decrease the deviation angles and improve the aerodynamics performance of cascade.
结果表明,附面层吸除能促进附面层减薄,减少分离损失,有助于降低叶栅总压损失,提高气流折转能力,改善叶栅气动性能。
参考词条
补充资料：CT导向肝囊肿抽吸与硬化剂治疗
CT导向肝囊肿抽吸与硬化剂治疗
介入放射学技术。在CT引导下穿刺肝囊肿，吸尽囊液，然后缓慢注入乙醇，硬化治疗肝囊肿的技术。穿刺时应避免误穿入血管、胆管或腹腔动脉。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。