Design Optimization of a Transonic-Fan Rotor Using Numerical Computations of the Full Compressible Navier-Stokes Equations and Simplex Algorithm

<table>Comparison between the current computations of the rotor pressure ratio and the measured NASA Rotor 67.</table>

International Journal of Rotating Machinery

fig11

Figure 11

Figure 11: Design Optimization of a Transonic-Fan Rotor Using Numerical Computations of the Full Compressible Navier-Stokes Equations and Simplex Algorithm 

Figure 11 | Design Optimization of a Transonic-Fan Rotor Using Numerical Computations of the Full Compressible Navier-Stokes Equations and Simplex Algorithm 