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Design method for turbomachine blades with finite thickness by the circulation method
Jun Jiang,
Thong Dang
Department of Mechanical & Aerospace Engineering
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Dive into the research topics of 'Design method for turbomachine blades with finite thickness by the circulation method'. Together they form a unique fingerprint.
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Keyphrases
Circulation Method
100%
Finite Thickness
100%
Turbomachine Blades
100%
Inverse Method
100%
Design Calculation
100%
Blade Shape
50%
Blade Geometry
50%
Pressure Loading
50%
Three-dimensional (3D)
50%
Blade Surface
50%
Analytical Solution
50%
Consistency Checking
50%
Incompressible Flow
50%
Panel Data Analysis
50%
Inviscid Flow
50%
Thickness Distribution
50%
Blade Thickness
50%
Tangency Condition
50%
Inverse Mode
50%
Inlet Guide Vane
50%
Turbine Blade
50%
Impulse Turbine
50%
Thin-walled Blade
50%
Compressor Blade
50%
Engineering
Inverse Method
100%
Design Method
100%
Turbomachine Blades
100%
Design Calculation
100%
Blade Surface
50%
Blade Thickness
50%
Blade Geometry
50%
Incompressible Flow
50%
Inviscid Flow
50%
Thickness Distribution
50%
Impulse Turbine
50%
Guide Vane
50%
Inverse Mode
50%
Compressor Blades
50%