turbine vane - Globe Thesis

Keyword [turbine vane] Result: 21 - 40 \| Page: 2 of 2
21.	Multidisciplinary Coupling Analysis For The Cooling Effects Of Gas Turbine Air-Cooling Vanes
22.	Research On The Flow And Heat Transfer Physics Of Novel Film Cooling Structures On The Leading Edge Of Turbine Blade
23.	Research On Contouring Method And Film Cooling Of Nonaxisymmetric Endwall In A Turbine Vane Cascade
24.	Investigation Of CMC’s Thermal Conduction Mechanism And Its Application In Thermal Analysis For Turbine Vane
25.	Investigation On The Film Cooling Mechanism Of Interrupted Slot With Step On The Turbine Vane Endwall
26.	Research On Aero-thermal Mechanism By Blended Blade And Endwall Technique Of Turbine Vane
27.	Study On The Influence Of Film Cooling Structure On The Cooling And Aerodynamic Performance Of High Press Turbine Vane
28.	Flow and heat transfer in an L-shaped cooling passage with ribs and pin fins for the trailing edge of a gas-turbine vane and blade
29.	Experimental Investigation of Particulate Deposition on a Simulated Film-Cooled Turbine Vane Pressure Surface in a High Pressure Combustion Facility
30.	Time-Averaged and Time-Accurate Aerodynamic Effects of Rotor Purge Flow for a Modern, Rotating, High-Pressure Turbine Stage and Low-Pressure Turbine Vane
31.	Cooling of a turbine vane endwall through contouring and flow injection
32.	Turbulence and three-dimensional effects on a film cooled turbine vane
33.	Detailed film cooling effectiveness and three component velocity field measurements on a first stage turbine vane subject to high freestream turbulence
34.	Study On The Heat Transfer And Film Cooling Characteristics Of The W Shaped Hole On A Turbine Vane
35.	Numerical Study On Cooling Performance Of Air-cooled Turbine Blade With Thermal Barrier Coating
36.	Enhanced Heat Transfer Mechanism And Performance Study On Composite Cooling Structure At Leading Edge Of A Gas Turbine Vane
37.	Investigation On The Flow And Cooling Performance Of The Film Cooling With Vortex Generators
38.	Multi-Objective Optimization Of Fan-Shaped And Round-To-Slot Holes Based On Discharge Coefficient And Cooling Effectiveness
39.	Study On Influence Of Blockage Of Film Cooling Holes Of Turbine Vane Pressure Surface
40.	Numerical Study On Cooling Performance Of Coated Blade By Rotor-stator Interference Under Hot Streak Effect
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