Fully three-dimensional viscous semi-inverse method for subsonic mixed-flow and radial impeller design

Keyphrases

• Blade Camber 20%
• Blade Geometry 20%
• Blade Shape 20%
• Blade Stacking 20%
• Blade Surface 40%
• Camber 40%
• Cost Reduction 20%
• Design Improvement 20%
• Design Procedure 20%
• Flow Field 20%
• GAS Process 20%
• Geometric Constraints 20%
• Grid Line 20%
• Impeller Design 100%
• Inverse Algorithm 20%
• Inverse Analysis 20%
• Inverse Design 20%
• Line Element 20%
• Manufacturing Process 20%
• Mechanical Integrity 20%
• Mixed-flow Impeller 100%
• Navier-Stokes Solver 20%
• New Design Approach 20%
• Pressure Loading 20%
• Process Application 20%
• Proposed Design 20%
• Radial Impeller 100%
• Reynolds-averaged Navier-Stokes 20%
• Semi-inverse 40%
• Semi-inverse Method 100%
• Span-wise 40%
• Stacking Line 20%
• Straight Line 20%
• Surface Design 20%
• Surface Smoothness 20%
• Three-dimensional (3D) 100%
• Time Marching 20%
• Turbomachinery 20%

Engineering

• Blade Geometry 33%
• Blade Surface 66%
• Blade Thickness 33%
• Cost Reduction 33%
• Design Method 66%
• Design Procedure 33%
• Flow Impeller 100%
• Flow Path 33%
• Grid Line 33%
• Impeller Design 100%
• Inverse Design Method 33%
• Inverse Method 100%
• Line Element 33%
• Manufacturing Process 33%
• Process Gas 33%
• Radial Impeller 100%
• Reynolds-Averaged Navier-Stokes 33%
• Straight Line 33%
• Turbomachinery 33%