Research Article
Modeling and Analysis of Shock Reduction through Counterflow Plasma Jets
Figure 13
Comparison of Mach contours at constant PR = 3, and = 1 also include changes in pressure with increasing Mach number. (a) = 1.4, (b) = 1.8, (c) = 2, and (d) = 3.
(a) |
(b) |
(c) |
(d) |