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Altitude Performance of a 20-Inch-Diameter Ram-Jet Engine Investigated in a Free-Jet Facility at Mach Number 3.0
| Content Provider | University of North Texas |
|---|---|
| Author | Smolak, George R. Wentworth, Carl B. |
| Organization | Lewis Flight Propulsion Laboratory |
| Description | Report discussing the performance of a 20-inch-diameter ram-jet engine at Mach number 3.0 over a range of simulated altitudes from 60,500 to 66,500 feet. Information about the maximum combustor efficiency, range of exhaust-nozzle total pressures, lean blow-out, diffuser total-pressure recovery, and internal thrust coefficient is provided. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc53178 |
| Language | English |
| Publisher Date | 2019-01-04 |
| Access Restriction | Open |
| Subject Keyword | aircraft engines aircraft performance ramjet engines |
| Content Type | Text |
| Resource Type | Report |