About 3801 item dissertation in line with TK4,Internal combustion engine query results,the following is 1 to 50(Search took 0.09 seconds)
- Research on Characteristics of Vortex Tube Air Intake Filter in Gas Turbine,HanJia/Harbin Engineering University,0/2
- The Numerical Simulation for Continuous Plasma Arc Generator Nozzle,YuZuoZuo/Harbin Engineering University,0/9
- Research on Mist/Air Cooling Enhancement Techniques of Turbine Blade,LiuRuiBao/Harbin Engineering University,0/9
- Research on the Technology of Gas Turbine Bearing Fault Diagnosis and Fault Prediction,LiuBingBing/Harbin Engineering University,0/18
- Research on Flow and Heat Transfer Mechanics at the Interaction of Conduction,Convection and Radiation on Gas Turbine Hot Component,WangWenPing/Tsinghua University,0/22
- Effects of Variable Geometry on Turbine Stage Performance,ZhangMingShuo/Harbin Engineering University,0/35
- Numerical Study of Blade Surface Curvature Effects on Film Cooling Performance,HuangYi/University of Shanghai for Science and Technology,0/17
- Numercal Study on Aerodynamic Performance of Mulyistage Gas Turbine with Cooling Air Mixing,WuYanLong/Harbin Institute of Technology,0/15
- Cooling System Improve and Numerical Simulation for the2ND Stage Rotor of Heavy-duty Gas Turbine,XueXingXu/Harbin Institute of Technology,0/29
- Effects of Reynolds Number on the Performance of Centrifugal Compressor,WangYunFei/Harbin Institute of Technology,0/82
- Numerical Study on Blade Cooling Structure Modification Design of High-pressure Turbine Rotor,LiChao/Harbin Institute of Technology,0/46
- Mechanism Study of Turbulent Cooling in a Gas Turbine,WangLongFei/Harbin Institute of Technology,0/86
- Research on Conjugate Heat Transfer Simulation of Gas Turbine Cooling Structure with Pipe-net Method,LiuMingLin/Harbin Institute of Technology,0/25
- Temperature Distribution of Turbine Blade and Establishment of Mathematical Model,ZhangXinYong/Harbin Engineering University,0/20
- The Control System Design of Gas Turbine Auxiliary Equipment,LiChong/Northeastern University,0/14
- Research on Mist/Air Film Cooling Enhancement Techniques of Plate,Zhang/Harbin Engineering University,0/16
- Loss Control Research of Adjustable Guide Vane in Variable Geometry Turbine,YuJian/Harbin Engineering University,0/19
- Numerical Simulation and Designation of Gas Turbine Combustion Test Section,NiLanKai/Harbin Engineering University,0/27
- Research on Performance of Flame Ignition and Extinction of Can Annular Combustor,LiYaJun/Harbin Engineering University,0/35
- Plasma Ignition System Simulation and Experimental Research,LiWenZuo/Harbin Engineering University,0/10
- Design and Numerical Prediction Research of Combustor Experiment Rig,KangZhenYa/Harbin Engineering University,0/20
- Numerical Study on Multi-physical Field of Plasma Ignition Generator,LiuYanYan/Harbin Engineering University,0/25
- A Research of Fuel Reforming and Combustion Technologies in Gas Turbine Combustor,LongQiang/Harbin Engineering University,0/29
- Numerical Prediction for Lean Blowout of Annular Combustion,ZhangZuo/Harbin Engineering University,0/42
- The Stability Analysis of Gas Turbine Ompression System,HanLei/Harbin Engineering University,0/19
- The Overal Performance Simulation Research on the Intercooled-cycle Gas Turbine,YingYuLong/Harbin Engineering University,0/25
- Dome Design and Numerical Simulation of Combustion Flow Field for a Triple Swirler Combustor,ZhangChenZuo/Harbin Engineering University,0/60
- Optimization Design of Cooling Structure in Low Pressure Turbine Blade,YaoJianHui/Harbin Engineering University,0/40
- The Numerical Investigation about Effects of Inlet Fogging on Rotating Stall in a Transonic Compressor Rotor,WangPengZuo/Harbin Engineering University,0/19
- The Design of the Variable Geometry Turbine Blade,JingXiaoXu/Harbin Engineering University,0/20
- Influence of Turbulent Fluctuation on Combustion Flow Field of Annular Combustion Chamber,TangZhongBin/Harbin Engineering University,0/41
- Research on Fault Diagnosis of Gas Turbine Bearing,WangQiang/Harbin Engineering University,0/33
- Dual Fuel Nozzle Design and Numercial Simulation of Combustion Flow Filed,HeHongBin/Harbin Engineering University,0/47
- Numerical Simulation of the Impact of Turbine Blade Film Cooling Caused by Hole Injection,SunShaoHai/Harbin Engineering University,0/45
- Off-design Performance Simulation Research of Chemically Recuperated Gas Turbine Cycle,LiuQingZhen/Harbin Engineering University,0/20
- Schematic Design and Parametric Optimization of the Air-blast Atomizing Duel-fuel Atomizer,HuXiaoMing/Harbin Engineering University,0/29
- Turbine Blade Temperature Measurement Base on LabWindows/CVI,ZhouZiLong/Harbin Engineering University,0/12
- Development of Vacuum Arc Cathode Target Materials for Coating,WangXu/Changchun University of Science and Technology,0/0
- Research for Fault Diagnosis and Simulation of Turbine Blades,LiuYingQian/Harbin Engineering University,0/45
- Study of Temperature Signal Feature Extraction Methods of Turbine Blade,GuanJingTao/Harbin Engineering University,0/25
- Research on the Mechanism of Flow and Heat Transfer in Rotor-stator Cavities in Gas Turbine,LinLi/Tsinghua University,0/36
- Model-based Gas Path Diagnostics for Heavy-duty Gas Turbine,PuXingXing/Tsinghua University,0/47
- Research on the Mechanism of Flow and Heat Transfer Interaction in Anisotropic Turbulent Film Cooling Flows,LiXueYing/Tsinghua University,0/18
- p-Multigrid Discontinuous Finite Element Method and Application for Gas Turbine's Cooling Flow,TanQinXue/Tsinghua University,0/36
- Conjugate Heat Transfer Mechanisms for Coal-Based-Fuel Gas Turbines,ZouZuo/Tsinghua University,0/9
- Improvement Research of Cooling Structure in Low Pressure Turbine Blade,YuFeiLong/Harbin Engineering University,0/6
- Analysis of the Rod-fastening Rotor's Distortion Similarity Problem and Research on a Characteristic Prediction Method,ChenJie/Central South University,0/9
- The Numerical Simulation of the Cold Flow Properties in the Advanced Vortex Combustor,TuGuoHui/Nanchang University of Aeronautics and,0/25
- Research of Turbine Blade Tip Clearance Measuring Technology Based on Capacitive Sensor,LiWeiShuang/Harbin Engineering University,0/29
- Research on Maintenance Interval Optimization Strategy Model of Gas Turbine Passage Parts,ChengYuan/Zhejiang University,0/38
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