Development of an improved streamline curvature approach for transonic axial compressor

Engineering

• Streamlines 100%
• Axial Compressors 100%
• Aerodynamics 33%
• Computational Fluid Dynamics 33%
• Flow Distribution 33%
• Design Condition 33%
• Characteristic Curve 33%
• Incidence Angle 33%
• Dimensional Flow 33%
• Pressure Loss 33%
• Performance Prediction 33%
• Design Stage 33%
• Internal Flow Field 33%
• Preliminary Design 33%
• Multistage Compressor 33%