SCRAMJET INJECTION
Jet injection into a supersonic cross flow is a basic way of introducing fuel into a supersonic combustor. Engines with supersonic combustors are needed for hypersonic vehicles with airbreathing propulsion. Shown here are some pictures of gaseous injection tests conducted at UCI a few years ago. It is hoped that these experiments will continue with liquid injection into a supersonic cross flow using our special mixing enhancement methods to distribute fuel evenly inside the combustor.
Cross-stream: Air at Mach 2.0
| Jet Mach number : | 1.0 | 2.1 | 2.8 | 3.5 |
| Momentum ratio | ||||
| 5.3 | Helium | Helium | Helium | Helium |
| 8.3 | Helium | Helium | Helium |
Cross-stream: Air at Mach 3.0
| Jet Mach number : | 2.1 | 2.8 |
| Momentum ratio | ||
| 3.0 | Helium | Helium |
| 5.3 | Helium |
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