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Parametric performance of a turbojet engine combustor using jet a and a diesel fuel
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Humenik, F. M. Butze, H. F. |
| Copyright Year | 1979 |
| Description | The performance of a single-can JT8D combustor was evaluated with Jet A and a high-aromatic diesel fuel over a parametric range of combustor-inlet conditions. Performance parameters investigated were combustion efficiency, emissions of CO, unburned hydrocarbons, and NOx, as well as liner temperatures and smoke. At all conditions the use of diesel fuel instead of Jet A resulted in increases in smoke numbers and liner temperatures; gaseous emissions, on the other hand, did not differ significantly between the two fuels. |
| File Size | 1449539 |
| Page Count | 45 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19790011943 |
| Archival Resource Key | ark:/13960/t2p60ch8r |
| Language | English |
| Publisher Date | 1979-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Performance Tests Exhaust Gases Hydrocarbons Nitrogen Oxides Air Pollution Smoke Carbon Monoxide Combustion Chambers Jet Engine Fuels Diesel Fuels Combustion Efficiency Turbojet Engines Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
