Preliminary Research on a High Thrust-to-Weight Ratio of Double-Sided Composite Impeller Microturbine Engine

Figure 19

Static pressure contours of turbine channel. (a) 0.1 span. (b) 0.3 span. (c) 0.5 span. (d) 0.7 span. (e) 0.9 span.

(a)

(b)

(c)

(d)

(e)