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Combustion-efficiency investigation of special fuels in single tubular-type combustor at simulated altitude conditions
| Content Provider | University of North Texas |
|---|---|
| Author | Dittrich, Ralph T. |
| Organization | Lewis Flight Propulsion Laboratory |
| Description | Report presenting a combustion-efficiency investigation of 10 special straight-run distillate fuels in an individual tubular-type combustor unit of a 14-unit assembly at two simulated engine operating conditions. These distillates were obtained from various crude oils and consisted of hydrocarbon mixtures with distillations temperature varying from 93 to 690 degrees Fahrenheit. Comparison of temperature measurements obtained from two locations in the exhaust duct showed that under certain operating conditions the flame extended beyond the turbine position. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc58042 |
| Language | English |
| Publisher Date | 2018-07-11 |
| Access Restriction | Open |
| Subject Keyword | aircraft combustors combustion efficiencies |
| Content Type | Text |
| Resource Type | Report |