Design of a Single Stage Centrifugal Compressor as Part of a Microturbine Running at 60000 rpm, Developing a Maximum of 60 kW Electrical Power Output

Engineering

• Computational Fluid Dynamics 50%
• Conservation of Energy 100%
• Conservation of Mass 50%
• Diffusers 50%
• Electrical Power 100%
• Flow Passage 50%
• Geometric Dimension 50%
• Impeller 100%
• Mass Conservation 50%
• Micro Gas Turbine 50%
• Microturbines 100%
• Momentum Conservation 50%
• Nonlinear Optimization 50%
• Permanent Magnet 50%
• Power Generation 50%
• Power Output 100%
• Radial Impeller 50%
• Single Stage Centrifugal Compressor 100%
• Small Gas Turbine 50%
• Stream Velocity 50%
• Volute 50%