Research Article
An Air Jet Distortion Generation System
Figure 7
Variation of (a) total pressure loss and (b) exit Mach number () as a function of mass flow ratio / for different values of inlet Mach number () with δM 1 = 0.05 obtained by inviscid analysis. The calculations were done for = 102 mm, four jets with d j = 7.5 mm.
| (a) |
| (b) |