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

<table>Typical blade thickness and blade camber line in blade-to-blade plane using Bezier curve.</table>

International Journal of Rotating Machinery

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Figure 6

Figure 6: Design Optimization of a Transonic-Fan Rotor Using Numerical Computations of the Full Compressible Navier-Stokes Equations and Simplex Algorithm 

Figure 6 | Design Optimization of a Transonic-Fan Rotor Using Numerical Computations of the Full Compressible Navier-Stokes Equations and Simplex Algorithm 