Blade leading edge - Globe Thesis

Keyword [Blade leading edge] Result: 1 - 20 \| Page: 1 of 2
1.	Investigation Of The Effects Of Incidence Angle And Film Hole Shape On Gas Turbine Vane Leading Edge Film Cooling
2.	An Experimental Investigation Of Flow Characteristics With Film Cooling Holes On Turbine Blade Leading Edge
3.	Experimental Investigation Of Film Cooling Efficiency On Turbine Blade Leading Edge
4.	Investigation On Film Cooling Performances In Turbine Blade Leading Edge
5.	Investigation On The Characteristics Of The Flow And Heat Transfer Of Turbine Blade
6.	Wind Turbine Blade Leading Edge Discrete Slot Of Film-forming Characteristic Research
7.	Research On The Ultrasonic Testing Of Wind Turbine Blade Leading Edge
8.	Investigation On The Characteristics Of Leading Edge Film Cooling Of Turbine Blade
9.	Effect Of Impeller Inlet Geometry On Cavitation Performance Of Centrifugal Pumps Based On Radial Basis Function
10.	Research On Flow And Heat Transfer Of Impingement Cooling In Turbine Blade Leading Edge With Crossflow
11.	Study On Film-forming Characteristics Of Vertical Axis Wind Turbine Blade Leading Edge To Open The Primary And Secondary Holes
12.	Measurement And Modeling Of Contour Profile Of Aeroengine Turbine Blades
13.	Investigation On Aerodynamic Performance Of Horizontal Axis Wind Turbine By Setting Micro-cylinder In Front Of The Blade Leading Edge
14.	Aerodynamic Analysis And Research Of Aeroengine Fan Blade Based On Wind Erosion
15.	Influence of blade leading edge geometry and upstream blowing on the heat/mass transfer in a turbine cascade
16.	The heat and mass transfer analogy factor, Nu/Sh for two-dimensional and three-dimensional boundary layers
17.	Numerical Investigations On Cooling Characteristics Of Turbine Blade Endwall And Leading Edge
18.	The Orifice-type Impinging Cooling Jet Applied Internally At Gas Turbine Blade Leading Edge
19.	Investigation On The Characteristics Of The Flow And Heat Transfer Of Turbine Guide Blade Film Cooling
20.	On The Fluid Flow And Heat Transfer Mechanism Of Cooling Structure Of Leading Edge In Gas Turbine Blade
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