Design method for turbomachine blades with finite thickness by the circulation method

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%