This facility allows for high speed internal flow and jet studies. The facility is capable of Mac nos ranging from subsonic to high supersonic in continuous mode. The open jet layout is modular allowing the inlet section to vary from 1 inch to 4 inches.
| Maximum mass flow rate | Maximum delivery pressure | This setup consists of |
|---|---|---|
| 1.2kg/s | 25 BAR | Tubes, settling chamber, honeycomb, wire mesh and nozzle mounting arrangement |
This setup can be used for aero-acoustic research and jet-related studies.
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