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Altitude performance of an-f-58 fuels in j33-a-21 single combustor
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1949 |
| Description | Three fuels conforming to AN-F-58 specification were investigated in order to determine the influence of boiling temperatures and aromatic content on altitude performance in single combustor of a 4600-pound-thrust turbojet engine. Combustion efficiencies of the three AN-F-58 fuels were approximately equal at each simulated engine condition for altitudes from 5,000 to 50,000 feet, 90-percent normal rated engine speed, and flight Mach numbers of 0.0 and 0.6. |
| File Size | 2138157 |
| Page Count | 25 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930085528 |
| Archival Resource Key | ark:/13960/t2n62w24n |
| Language | English |
| Publisher Date | 1949-04-08 |
| Access Restriction | Open |
| Subject Keyword | Fuels - Physical Properties Combustion - Effect OF Engine Operating Conditions AND Combustion-chamber Geomet Fuels - Relation To Engine Performance Combustion - Turbine 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 |
