Research Article

Effects of Different Blade Angle Distributions on Centrifugal Compressor Performance

Figure 3

Contours of nondimensional wall distance y for case at the design mass flow rate with the k- -SST turbulence model. Values at the pressure side (PS) are plotted from the leading edge to the trailing edge along the blade surface (highlighted white spots).
537802.fig.003a
(a)
537802.fig.003b
(b)