Tip clearance flow is one of the most important resources of losses in turbine rotors.
叶顶间隙流动是导致涡轮动叶中产生流动损失的主要原因之一。
Experimental study on the pressure in the balance cavity of floating impeller;
浮动叶轮平衡腔压力的试验分析
NUMERICAL SIMULATION OF SHOCK SYSTEMS IN CONVERGINGDIVERGING NOZZLE ROTOR TURBINE STAGE WITH DIFFERENT OUTLET STATIC PRESSURE
背压对缩放型流道涡轮动叶激波结构的影响
disc ,rotor (with or without fins) for turbojet engines
叶轮（带或不带叶片）,用于涡轮喷气发动机
Large eddy simulation of separated flow transition on a highly-loaded low pressure turbine profile
大负荷低压涡轮叶型分离转捩流动的大涡模拟
AN INVESTIGATION ON AERODYNAMIC PERFORMANCE OF A VANELESS COUNTER-ROTATING TURBINE WITH RECESSED HIGH-PRESSURE ROTOR TIPS
无导叶对转涡轮高压动叶叶尖开槽的研究
a turbine that is driven by jets direct against the blades.
喷气机直接对准浆叶驱动的涡轮。
This steam is used to turn turbine blades of electric generators.
这蒸汽被用来推动发电机的涡轮叶片。
Aerodynamic performance of a highly-loaded low-pressure turbine profile
一种大负荷低压涡轮叶型的气动性能
Influence of Axially-swept Blades on the Aerodynamic Performance of a Turbine Stationary Cascade
轴向掠对涡轮静叶栅气动性能的影响
blade, for gas turbines (excl. turbopropellers)
叶片，用于燃气轮机（不包括涡轮螺旋桨发动机）
Numerical Investigation on Pressure Fluctuations Induced by Interblade Vortices in a Runner of Francis Turbine
混流式水轮机转轮区叶道涡压力脉动数值研究
Effects of endwall relative motion on tip clearance flow in turbine rotors
机匣相对转动对涡轮叶顶间隙流动的影响
SIMULATION OF EFFECTS OF BLADE ROTATION ON TIP CLEARACNE FLOW IN AXIAL TURBINES
叶片转动对涡轮间隙内部流动影响的数值研究
Research on Aero-engine Blade Containment Test and Computational Simulation;
航空发动机涡轮叶片的包容试验和数值仿真
Analysis of Stress and Vibration of Blade for Aero Turbocharger
小型航空涡轮增压器叶片强度振动研究
Numerical Research of Tip Clearance Flow Structure in a Pivoting-Stator of Radial Inflow Turbines
向心涡轮可调导叶间隙流动的数值研究
A Numerical Simulation Consideration an Exhaust Gas Turbine Stage Cascade with Tip Clearance
计及动叶顶部间隙影响的烟气涡轮数值模拟
Effect of different incidences on turbine cascades flow in blade tip clearance
冲角变化对涡轮叶栅内间隙流动的影响
Numerical Investigation of Air-cooled Gas Turbine Flow and Thermal Stress Characteristics
气冷涡轮叶栅流动及热应力特性的数值研究