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Effects of fuel-nozzle carbon deposition on combustion efficiency of single tubular-type, reverse-flow turbojet combustor at simulated altitude conditions
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1948 |
| File Size | 14432681 |
| Page Count | 30 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082339 |
| Archival Resource Key | ark:/13960/t02z5k21c |
| Language | English |
| Publisher Date | 1948-06-01 |
| Access Restriction | Open |
| Subject Keyword | Engines, Turbojet - Combustion Chambers Engines, Turbojet - Performance Effect OF Altitude Nozzles, Fuel-injection - Engines, Jet Engines - Carbon Deposits Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |