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Combustion performance of two experimental turbojet annular combustors at conditions simulating high-altitude supersonic flight (Document No: 19630003987)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1954 |
| Description | Performance of experimental annular turbojet combustors at simulated high altitude supersonic flight conditions |
| File Size | 2305809 |
| Page Count | 28 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19630003987 |
| Archival Resource Key | ark:/13960/t1vf1727v |
| Language | English |
| Publisher Date | 1954-03-26 |
| Access Restriction | Open |
| Subject Keyword | Combustor High Altitude Combustion Efficiency Turbojet Engine Simulated Altitude Supersonic Speed Flight Simulation 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 |