Performance sensitivity analysis and aerodynamic optimization of compressor cascades by a turbulence adjoint method

Engineering

• Aerodynamics 100%
• Two Dimensional 100%
• Flow Distribution 100%
• Blade Profile 100%
• Design Optimization 50%
• Aerodynamic Design 50%
• Reynolds-Averaged Navier-Stokes 50%
• Computational Cost 50%
• Performance Improvement 50%
• Design Parameter 50%
• Aerodynamic Performance 50%
• Partial Differential Equation 50%
• Equation Turbulence Model 50%