high-pressure turbine - Globe Thesis

Keyword [high-pressure turbine] Result: 41 - 58 \| Page: 3 of 3
41.	Structure Optimization Design Of Aero-engine Turbine Disk Under Fatigue Constraints
42.	Study On The Influence Of Tip Coolant Injection On Turbine Blade Tip Flow And Heat Transfer
43.	Three-dimensional unsteady simulation of a modern high pressure turbine stage: Analysis of heat transfer and flow
44.	The influence of film cooling and inlet temperature profile on heat transfer for the vane row of a 1-1/2 stage transonic high-pressure turbine
45.	Experimental and computational investigation of inlet temperature profile and cooling effects on a one and one-half stage high-pressure turbine operating at design-corrected conditions
46.	Influence of loading distribution on the performance of high pressure turbine blades
47.	Time-Averaged and Time-Accurate Aerodynamic Effects of Rotor Purge Flow for a Modern, Rotating, High-Pressure Turbine Stage and Low-Pressure Turbine Vane
48.	An experimental investigation of clocking effects on turbine aerodynamics using a modern 3-D one and one-half stage high pressure turbine for code verification and flow model development
49.	Entropy generation in the tip region of a high-pressure turbine
50.	Stability Analysis Of Wake Generation Mechanisms And Its Applications In Turbine Flow
51.	Modernization Of Cooling System Of The High-pressure Turbine Blade For Bypass Turbofan Engine
52.	Multiphysics Coupling Analysis And Cooling Structure Optimization Design Of High-pressure Turbine Blades
53.	Research On The Influence Of Manufacturing Error Of Mounting Edge Of Bolt-stop Connection On The Assembly Performance
54.	Research On Heat Transfer Characteristics Of High Pressure Turbine Blade
55.	Multifield Coupling Analysis Of The Influence Of Labyrinth Clearance On Temperature Field Of High Pressure Turbine Rotor
56.	Effect Of Probe Measuring Layout On Turbine Aerodynamic Performance
57.	The Numerical Simulation Of Effect Of Non-uniform Flow Of High Pressure Turbine Inlet
58.	An Analysis Of The High-Temperature Highpressure Turbine Working Blades Cooling System For Next-Generation Gas Turbine Engines
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