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Cooling characteristics of a transpiration-cooled afterburner with a porous wall of brazed and rolled wire cloth
| Content Provider | University of North Texas |
|---|---|
| Author | Koffel, William K. |
| Organization | Lewis Flight Propulsion Laboratory |
| Description | Report presenting cooling data for a transpiration-cooled afterburner with a porous combustion-chamber wall of brazed and and rolled wire cloth for a range of exhaust-gas temperatures, total flow ratios of cooling air to combustion gas, and pressure altitudes. Results regarding typical data, cooling correlation, transpiration-cooling performance, comparison of transpiration and forced-convection cooling, and pressure environment of the wire cloth are provided. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc62507 |
| Language | English |
| Publisher Date | 2018-06-04 |
| Access Restriction | Open |
| Subject Keyword | aircraft afterburners pressure characteristics |
| Content Type | Text |
| Resource Type | Report |