Research Article
Design of a Three-Dimensional Hypersonic Inward-Turning Inlet with Tri-Ducts for Combined Cycle Engines
Table 4
Mass-averaged performance of the tri-duct inlet at
and 1.2.
| | Mass flow ratio | Total pressure recovery | Exit Mach number | Exit pressure ratio |
| 2 | T | 0.06 | 0.48 | 0.56 | 2.93 | E | 0.32 | 0.84 | 1.52 | 1.68 | S | 0.21 | 0.89 | 1.60 | 1.61 |
| 1.2 | T | 0.06 | 0.76 | 0.53 | 1.47 | E | 0.25 | 0.90 | 0.84 | 1.38 | S | 0.15 | 0.89 | 1.16 | 0.92 |
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