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

<div>Static temperature field contours. (a) Static temperature field contour of the DSCI. (b) Static temperature field contour the turbine outside.</div>

International Journal of Aerospace Engineering

fig24

Figure 24

Figure 24: Preliminary Research on a High Thrust-to-Weight Ratio of Double-Sided Composite Impeller Microturbine Engine 