Research Article
An Air Jet Distortion Generation System
Figure 6
Distortion parameters at the AIP for four jets with unequal mass flow rates āā. In this figure (a) contours of total pressure loss ], (b) distribution of total pressure loss in each of the five rings, (c) contours of Mach number, (d) Mach number distribution in the five rings, (e) the circumferential distortion parameter IDC, and (f) the radial distortion parameter IDR in the rings.
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