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An assessment of the use of antimisting fuel in turbofan engines
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Desaro, R. Franz, T. Fiorentino, A. |
| Copyright Year | 1980 |
| Description | The effects of antimisting kerosene on the performance of the components from the fuel system and the combustor of a JT8D aircraft engine were evaluated. The problems associated with antimisting kerosene were identified and the extent of shearing or degradation required to allow the engine components to achieve satisfactory operation were determined. The performance of the combustor was assessed in a high pressure facility and in an altitude relight/cold ignition facility. The performance of the fuel pump and control system was evaluated in an open loop simulation. |
| File Size | 12536561 |
| Page Count | 147 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810010789 |
| Archival Resource Key | ark:/13960/t1kh5d640 |
| Language | English |
| Publisher Date | 1980-11-01 |
| Access Restriction | Open |
| Subject Keyword | Propellants And Fuels Performance Tests Nozzle Flow Kerosene Hydrocarbon Fuels Turbofan Engines Aircraft Engines Combustion Chambers Fuel-air Ratio 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 |
