Research Article

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

Figure 26

Flow path at different sections near the blade tip leading edge.
743154.fig.0026a
(a) 90% Span
743154.fig.0026b
(b) 95%
743154.fig.0026c
(c) 100%