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

Figure 17

Blade-to-blade planes of double-sided centrifugal compressor for relative Mach number. (a) 0.1 span. (b) 0.5 span. (c) 0.9 span.

(a)

(b)

(c)